Deutscher Luft- und Raumfahrtkongress 2007 - CEAS 2007

Preliminary Programme 

www.CEAS2007.org CEAS@DGLR.DE

Imprint 

Editor 

Deutsche Gesellschaft für Luft- 

und Raumfahrt - Lilienthal- 

Oberth e.V. German Society 

for Aeronautics and 

Astronautics (DGLR) ® 

Godesberger Allee 70 

D-53175 Bonn 

Phone: +49 (0228) 30 805-0 

Fax: +49 (0228) 30 805-24 

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http://www.dglr.de 

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Editorial Staff 

Dr. Irene Lopez 

Ferdi Olbert

Deutscher Luft- und Raumfahrtkongress 2007 

CEAS 2007 

1st European Air and Space Conference 

Century Perspectives 

Berlin, 10. – 13. September 2007

Index of Contents 

Foreword by Prof. Dr.-Ing. Joachim Szodruch, President of the DGLR Page 5 

Foreword by Sir Colin Terry, President of CEAS Page 7 

Foreword by Klaus Wowereit, Governing Mayor of Berlin Page 9 

Programme Committee Page 10 

Young Professionals Conference (DGLR-Nachwuchstagung) Page 11 

Conference Overview Page 12 

Detailed Technical Programme Page 14 

Poster sessions Page 38 

DGLR-Short Course Aircraft Design Page 41 

General Information Page 43 

Social Programme and Accompanying Persons Programme Page 47 

Technical Tours Page 49 

Choice of pre-reserved Hotels Page 50 

City Map of Berlin with Hotels and Venue Page 51 

Supporter of the Congress Page 52 

Host and Organizer 

Host of the Conference 

Deutsche Gesellschaft für Luft- und Raumfahrt - Lilienthal-Oberth e.V. 

German Society for Aeronautics and Astronautics (DGLR) 


D-53175 Bonn 

Phone: +49 (0228) 3 08 05-0 

Fax: +49 (0228) 3 08 05-24 

Internet: http://www.dglr.de 

Organizer of the Conference 

machtWissen.de AG 

Fahrenheitstraße 1 

D-28359 Bremen 

Phone: +49 (0421) 2208 266 

Fax: +49 (0421) 2208 267 

Internet: http://www.machtwissen.de 

Register: Bremen, HRB 23746 

4

Foreword by Prof. Dr.-Ing. Joachim Szodruch, President of the DGLR 

It is a great pleasure for me to present you the first congress of the Council of the European Aerospace 

societies (CEAS). CEAS currently comprises the eight aerospace societies from France, Germany, 

Great Britain, Italy, the Netherlands, Spain, Sweden and Switzerland with more than 25.000 

individual members. Each society represents the leading national society in the field of aeronautics 

and astronautics. 

As the CEAS mission is to strengthen European alliances and working relationships between industries, 

universities and research establishments, the biannual European Air & Space Conference has 

been founded to provide a forum for presentation and discussion of all scientific and technical areas 

related to aeronautics and astronautics. CEAS wants to be a forum and as such would like to provide 

opportunities for European scientists and engineers to learn and exchange about new discoveries in 

aerospace science, technology and products. Furthermore we offer a place to discuss ideas and experiences 

and to develop a highly professional network free from cultural, political and ideological 

constraints. As in 2007 the presidency of the European Commission is being held by Germany, CEAS 

also wants to send out a signal in holding this first of a series conference in Berlin as a new start to 

gather the European aerospace societies, while opening up globally as well. 

In this context it is a great honour for the German Society for Aeronautics and Astronautics (DGLR), 

which is – at 95 years – the second oldest aerospace society in Europe, to host this conference as the 

local organizer. In order to demonstrate the very close relation between the DGLR and CEAS, we 

integrated our annually national aerospace conference this year into CEAS. Berlin was chosen as the 

place of the conference because of its long tradition in aeronautics. Otto Lilienthal did his first steps in 

aeronautics in and near Berlin, and the German institutional aeronautical research started about at the 

same time in Berlin and Göttingen exactly 100 years ago. In the beginning of the modern era of flight, 

several European companies settled in Berlin Adlershof to use the then recently founded research 

facilities. Also the first steps in rocket technologies have been taken in Berlin. 

5

As we continue into the 21st century, the aeronautical and space technologies will significantly con- 

tribute to evolution and growth within an evolving and changing global environment. Therefore, the 

2007 Congress in Berlin will have the theme: 

CENTURY PERSPECTIVES 

The focus of the presentations will follow the five goals of our Congress: 

• Access to space and future space utilization, 

• Innovative concepts for future air transport, 

• Environment and technologies for environmental aspects in aeronautics and space, 

• International cooperation among academia, research and industry, 

• Education and training for aeronautics and space; attracting young engineers. 

As this is the first Congress of CEAS, the prestigious event is gaining increasing recognition in the field 

of aeronautics. We are therefore very proud to present a technical program with more than 500 highquality 

papers and a series of lectures held in 12 parallel sessions. A speciality about this congress will 

be a short course about aircraft design held on three days, several workshops about astronautics, and 

a symposium for young scientist. I have no doubt that, for everyone participating in the Congress, it 

will be a valuable meeting to remember. 

This congress would not have been possible without your engagement, so I would like to extend my 

sincere thanks to the Programme Committee, the local organizers, to all authors who are sharing their 

work and ideas with us as well as to all session chair persons who are bringing in their expertise, and 

especially also to you, the participants. 

I wish you all a very successful and fruitful meeting within a truly European and international environment. 

6

Foreword by Sir Colin Terry, President of CEAS 

It is a pleasure to welcome you to the first European Air and Space Conference in Berlin – the first 

conference organised by the newly constituted Council of European Aerospace Societies (CEAS). The 

Council brings together the major aerospace societies from across Europe and today is comprised of 

the Societies from France, Germany, Italy, Netherlands, Spain, Sweden, Switzerland and the United 

Kingdom. 

The conference here in Berlin is focussed on the technological challenges facing aeronautics in the 

coming years and brings together experts from a wide range of technical disciplines. I hope that the 

presentations of subsequent discussions will provide an ideal platform for Europe to build upon its 

previous successes in this important industry. In particular the focus on the current challenges including 

the environment and future space utilisation mean that there is much for delegates to digest. 

I would like to thank the DGLR for their organisation of the conference and also to thank the Programme 

Committee whose substantial efforts have made this event possible. 

I hope that you enjoy your time in Berlin and it proves to be a valuable meeting that shapes the future 

of aeronautics in Europe. 

7

Intentionally left blank 

8

Foreword by Klaus Wowereit, Governing Mayor of Berlin 

I am delighted to welcome all of you attending the 1st CEAS European Air and Space Conference to Germany’s 

capital city. It is a great honor for Berlin, as an international trade fair and congress venue, to be hosting your 

important conference. I also regard your choice as a tribute to Berlin-Brandenburg as a business and science 

location with much expertise in the area of aeronautics and astronautics. 

After all, the capital city region was not only the birthplace of German aviation, but has also been able to con- 

tinue this tradition. Today the aeronautics and astronautics industry is among the most promising sectors in our 

region. A number of global players are active here, along with many small and medium-size businesses and 

countless research institutes focusing on areas important to aeronautics and astronautics. In addition, Berlin is 

home to one of the world’s biggest air shows, the international aerospace exhibition ILA. With the opening of 

our new major airport, Berlin Brandenburg International, planned for 2011, the region’s aviation industry will 

take off to new heights. 

I am thus all the more pleased that the Council of European Aerospace Societies (CEAS) has chosen Berlin as 

the venue for this conference. With the 1st CEAS European Air and Space Conference, you are underscoring our 

reputation as an aeronautics and astronautics location with excellent prospects. 

I wish all of the participants a productive meeting and a very pleasant stay in Germany’s capital city. I hope you 

will also find the time to explore Berlin’s cultural treasures and some of its many other sightseeing attractions. 

In this spirit, let me say once again: Welcome to Berlin! 

9

Programme Committee 

Board of Programme Committee 

Dr.-Ing. Detlef Müller-Wiesner, France (Chair) 

Prof. Dr.-Ing. Dieter Schmitt, France 

Prof. Dr.-Ing. Klaus Brieß, Germany 

Prof. Dr.-Ing. Robert Luckner, Germany 

Dr. Constantinos Stavrinidis, United Kingdom 

Mr. Alain Garcia, France 

Dr.-Ing. Dietrich Knoerzer, EC 

Members of Programme Committee 

Aviation 

Dipl.-Ing. Jan Schumacher, Germany 

Dr. eng. Ryszard Szczepanik, Poland 

Mr. Jean-François Georges, France 

Mr. Claude le Tallec, France 

Mr. Angel Luis Arias, Spain 

Prof. V. E. Fortov, Russia 

Dr. Andreas Geisler, Austria 

Manned Aircraft 

Prof. Dr.-Ing. Dieter Scholz, Germany 

Dr. eng. Tomasz Goetzendorf-Grabowski, Poland 

Mr. Francois Jouaillec, France 

Mr. Yaakko Hoffren, Finnland 

Unmanned Aerial Systems 

Dipl.-Ing. Wolfgang Engelhardt, Germany 

Prof. Dr. Zdobyslaw Goraj, Poland 

Dr. Jan-Floris Boer, The Netherlands 

Mr. Floor Pieters, The Netherlands 

Mr. Manuel Mulero, Spain 

Dr. Georges Bridel, Switzerland 

Space Systems 

Prof. Dr.-Ing. Klaus Brieß, Germany 

Prof. Zbgniew Klos, Poland 

Mr. Christophe Bonnal, France 

Mr. Paul Kamoun, France 

Mr. Pat Norris, United Kingdom 

Mr. Koos Prins, The Netherlands 

Mr. M. Bandecchi, The Netherlands 

Mr. E. Kircher, The Netherlands 

Prof. P. Gaudenzi, Italy 

Mr. Thierry Leveugle, Spain 

Utilization of Space Environment 

Dr. rer.nat. Peter Vits, Germany 

Mr. Zeholij Pronk, The Netherlands 

Prof. C. Buongiorno, Italy 

Dr. G. Schwehm, The Netherlands 

Prof. O. Alifanov, Russia 

Fluid Dynamics and Thermodynamics 

Dipl.-Ing. Gregor A. Dirks, France 

Prof. Piotr Doerffer, Poland 

Prof. Piotr Wolanski, Poland 

Mr. Jean Delery, France 

Dr. W. Kordulla, The Netherlands 

Prof. M. Onofri, Italy 

Dr. Salvatore Borrelli, Italy 

Mr. Sergely Leonidowitsch Chernyshev, Russia 

Aerospace Propulsion 

Prof. Dr.-Ing. Rainer Walther, Germany 

Prof. Rudolf Klemens, Poland 

Mr. Pierre-Guy Amand, France 

Mrs. Isabelle Dubois, France 

Mr. Denis Arrat, France 

Prof. Dr.-Ing. Stephan Staudacher, Germany 

Prof. Jim McGuirk, United Kingdom 

Mr. Oscar Kogenhop, The Netherlands 

Mr. G. Saccoccia, The Netherlands 

Mr. U. Palmnas, Sweden 

IInformation´s Technology and Electronics 

Dr.-Ing. Thomas Wittig, Germany 

Dr. eng. Andrzej Homziuk, Poland 

Mr. Gilles Moury, France 

Mr. J. Bosma, The Netherlands 

Flight Guidance and Control Flight Mechanics 

Prof. Dr.-Ing. Robert Luckner, Germany 

Prof. Janusz Narkiewicz, Poland 

Mr. Angel Mateo, Spain 

Mr. Uwe Feucht, Germany 

Dr. Jörg Wildi, Switzerland 

Spacecraft Structures, Materials & Mechanical Testing 

(SSMMT) 

Prof. Dr. Michael Sinapius, Germany 

Prof. Dr. Horst Baier, Germany 

Prof. (em) Dr. Michael Link, Germany 

Dr. Michael Gaedke, Germany 

Dr. Jean Noel Bricout, France 

Mr. Torben Henriksen, The Netherlands 

System Management and Electronics 

Dipl.-Ing. Joachim Majus, Germany 

Prof. Cezary Szczepanski, Poland 

Mr. Brian Perry, United Kingdom 

Mr. Philippe Guay, France 

Mr. Pierre Tastet, France 

Mr. A. Massoni, France 

Air and Space Law 

Prof. Dr. jur. Stephan Hobe, Germany 

Prof. Kowaleczko, Poland 

Mr. Alexandre Korakis, France 

Aviation and Space Medicine 

Prof. Dr. med. Helmut Landgraf, Germany 

Dr. hab. med. Wieslaw Kowalski, Poland 

Mr. Claude Alexandre, France 

Aircraft Cabin and Cargo Systems 

Dr. K. Dieter Kricke, Germany 

Prof. Helen Muir, UK 

Mr. Lars Jonson, Sweden 

Dr. Gordon Konieczny, Germany 

Mechanical Flow Technology Study Group (STAB) 

Dr.-Ing. Hans-Joachim Heinemann, Germany 

Structures 

Prof. Dr.-Ing. Heinz G. Hönlinger, Germany 

Dr. eng. Cezary Galinski, Poland 

Mr. P. M. Hutin, France 

Mr. Jean-Noel Bricout, France 

Dr.-Ing. Jaap F. M. Wiggenraad, The Netherlands 

Mr. Henk Jan ten Hoeve, The Netherlands 

Mr. M. Lacoste, France 

Mr. Olli Saarela, Finnland 

Prof. Dr. Antonio Viviani, Italy 

Aviation and Space History 

Dipl.-Ing. Helmut Schubert, Germany 

Dr. eng. Piotr Zalewski, Poland 

Mr. Philippe Jung, France 

10

First CEAS European Air and Space Conference – 

Century Perspectives 

On the 11 th of September the German Society for Aeronautic 

and Astronautics (DGLR) invites groups from grammar schools, 

Secondary Schools or technical colleges to join the Deutscher 

Luft- und Raumfahrtkongress / 1 st European Air and Space 

Conference. 

Interested parties please contact: 

Carsten Holze 

DGLR, NWK-NK 

c/o machtWissen.de AG 

Fahrenheitstraße 1 

28359 Bremen 

Tel.: 0421 / 2208-266 

Fax.: 0421 / 2208-267 

E-Mail: carsten.holze@machtwissen.de 

11

Conference Overview 

Monday, September 10 th 

13:30 Press Conference Room Paris 

15:00 Opening Ceremony ECC Hall A 

20:00 Congress Reception of the Senate Rathaus Berlin 

19:00: Bus shuttle 

from Estrel-Hotel 

Tuesday, September 11 th 

08:30 Plenary Session ECC Hall C 

09:40-18:10 Lectures: Detailed technical programme see page 14 ff 

19:00 Parliamentary Evening ECC Hall A 

Wednesday, September 12 th 



19:30-24:00 Conference Dinner ECC Hall A 

Thursday, September 13 th 



20:00 Public Lecture by ESA Astronaut ECC Hall C/D 

and Member of DGLR Board: Thomas Reiter 

12

Lunch Arrangements 

Tuesday, 11.09.2007, to Thursday, 13.09.2007, 

Lunch is available (not included in registration fee) in the Estrel Hotel 

You can choose to eat à la carte in one of the 4 Restaurants belonging to the Estrel Hotel: 

"- Sun Thai, - Portofino, - La Patisserie, - Sansoucci" 

or have a small snack in the foyer of the lecture halls 

Coffee Breaks 

Tuesday, 11.09.2007, to Thursday, 13.09.2007, 

- Morning: 11:00 hrs - Afternoon: 16:30 hrs 

Those refreshments (Coffee or tea and cookies in the afternoon) are included in the congress fee. 

The Estrel-Hotel will offer additional soft drinks and pastries/snacks (not included in registration fee). 

13

Tuesday, 11th September 2007 

08:30- 

09:30 

Space Agencies Forum (Programmes) 

09:40 – 10:00 10:00 – 10:20 10:20 – 10:40 10:40 – 11:00 

Detecting and Characterising Aircraft Wake Vortices 

Chair: F. Holzäpfel, DLR Oberpfaffenhofen, DE 

Acoustic Characterisation and 

Localisation of Aircraft Wake 

Vortices 

U. Michel, Deutsches Zentrum für 

Luft- und Raumfahrt, DE; 

P. Böhning, Rolls-Royce 

Deutschland, DE 

Advanced Metallic Aerostructures 

Chair: P. Horst, TU Braunschweig, DE 

Development of Short Distance 

Welding Concepts for 

Airframes - WEL-AIR 

D. Alléhaux¹; F. Palm¹; I. 

Bordesoules, ALCAN, FR; M. 

Kocak, GKSS, DE; E. Gratiot, 

Dassault Aviation, FR; G. 

Troiano, ALENIA, IT; 

¹EADS IW, FR 

Comparison Between Arrival 

and Departure Wake Vortex 

Statistics Near the Ground 

F. Wang; S. Mackey; USDOT 

Volpe Center, US 

Magnesium for Aeronautic 

Structures 

E.H. Hombergsmeier, EADS 

Deutschland GmbH, DE 

Flight Guidance and Control: UAV Formation Flight & Refueling 

Chair: J. Wildi, RUAG Aerospace, CH 

Validierung der 

flugmechanischen 

Modellierung einer Luft-zu- 

Luft-Betankung mittels 

Flugtestdaten 

J.F. Beck¹; O.H. Heller, 

Eurocopter, FR; E. Özger¹; 

¹EADS, DE 

Autonomous UAV Refueling 

System 

B. Landkof; R. Zickel; D. 

Weinstein; V. Niazov; Technion, 

Faculty Aerospace Engineering, 

IL 

Ground-based and Air-borne 

LIDAR for Wake Vortex 

Detection and Characterisation 

A. Wiegele; S. Rahm; T. Gerz; 

German Aerospace Center, DE 

Potential Benefits of Integrally 

Stiffened Aircraft Structures 

L.U. Hansen; S. Häusler; P. 

Horst; Inst. für Flugzeugbau und 

Leichtbau, TU Braunschweig, DE 

Control Laws for UAV 

Formation Flying 

M. Chiaramonti; G. Mengali; 

University of Pisa, IT 

ECC Hall C 

Wake Vortex Data Collection 

and Analysis Using X-Band 

RADAR 

U. Meier, THALES Defence 


ECC Hall D 

Laser Beam Welding for A380 

family – From the first idea to 

an industrial process 

T. Behrens, Airbus Deutschland, 

DE 

Estrelsaal B 

Fuel Consumption Reduction 

for Unmanned Aerial Vehicles 

by Preplanned Formation 

Flights Using Mixed Integer 

Programming 

T. Kopfstedt; J.W. Vervoorst; 

Diehl BGT Defence, DE 

14 

11:20 – 11:40 11:40 – 12:00 12:00 – 12:20 12:20 – 12:40 

Controlling and Attenuating Wakes and Wake Encounters 

Chair: S.R.L. Lang, Federal Aviation Administration, US 

Automated Pilot Assistance for 

Wake Vortex Encounters 

C.W. Schwarz; K.-U. Hahn; DLR, 

DE 

Structures: Aeroelastics 

Chair: P.M. Hutin, ONERA, FR 

Calculation of Unsteady Loads 

for the F/A-18 Vertical Tail 

Buffeting 

M. Guillaume, RUAG Aerospace, 

CH; J. Vos, CFS Engineering, 

CH 

Wake Vortex Alleviation by 

Differential and Oscillating 

Flap Setting: A Comparative 

Numerical and Experimental 

Study 

G. Voß; E. Stumpf; R. Konrath; 

C.F. v. Carmer; DLR, DE 

Design and Analysis of an 

Aeroelastic Validation 

Experiment for Moving Flexible 

Airfoils 

R. Unger; J. Kleinert; M.C. Haupt; 

P. Horst; J. Windte; S. Bansmer; 

C.J. Kähler; R. Radespiel; 

TU Braunschweig, DE 

HMI - Displays 

Chair: V. Gollnick, TU Hamburg-Harburg, DE 

Method for Optimizing the 

Man-Machine Interface at 

Aircraft 

C.J. Szczepanski, Air Force 

Institute Of Technology, PL 

Simulation and Optimisation of 

Cockpit Display Visibility 

D.D. Dreyer, EADS Innovation 

Works, DE 

Fundamental Vortex 

Phenomena: Instabilities and 

Interactions with Jets and 

Wakes 

H.T. Schoenfeld¹; J.F. 

Boussuge¹; S. Le Dizès²; T. 

Leweke²; 

¹CERFACS, FR; ²CNRS-IRPHE, 

FR 

Aeroelastische 

Untersuchungen an 

nachgiebigen Tragflächen 

G. Thwapiah; L.F. Campanile; 

Empa, CH 

Enhanced Airport Situational 

Awareness by Airport Moving 

Map and Electronic Pre-Flight 

Information Bulletin 

C. Vernaleken; C. Urvoy; K. 

Koch; U. Klingauf; Technische 

Universität Darmstadt, DE 

ECC Hall C 

Wake Vortex Results from the 

AWIATOR Project 

A.C. de Bruin, NLR, NL; G. 

Schrauf¹; J. König¹; 

¹Airbus, DE 

ECC Hall D 

New Aerodynamic Modelling 

for Aeroelasticity in an 

Industrial Environment 

N. Forestier, Dassault-Aviation, 

FR 

Estrelsaal B 

The new Tornado Mission 

Support System in the 

Context of Network Centric 

Operations 

G. Gorgon, EADS, DE


08:30- 

09:30 


09:40 – 10:00 10:00 – 10:20 10:20 – 10:40 10:40 – 11:00 

Aerodynamics Aero-Engine Components 

Chair: R. Walther, MTU Aero Engines, DE 

New Concept of Test Section 

for Modeling of Flow on the 

Suction Side of Gas Turbine 

Blade 

P. Flaszynski, Gdansk University 

of Technology, PL; P. Doerffer, 

Institute of Fluid Flow Machinery 

PAN, PL 

Space Systems-Programmatic Aspects 

Chair: TBD 

Aligning Strategy with 

Capabilities: Towards a 

European Space Research 

Community 

A. Boese, DLR, DE 

Young Professional Conference I 

Chair: TBD 

Combustor Liner Temperature 

Prediction: A Preliminary Tool 

Development and its 

Application on Effusion 

Cooling Systems 

A. Andreini, Università di Firenze, 

IT 

The On-Orbit-Verificationprogramme 

of the German 

Space Agency 

P.G. Willemsen, M. Turk; 

R. Dittmann; 

German Aerospace Center - 

Space Agency, DE 

Determination of Aerodynamic 

Damping from Axial- 

Compressor-Blades Using a 

Bidirectional Fluid-Structure- 

Simulation 

S. Schrape; A. Kühhorn; J. 

Nipkau; BTU Cottbus, LS 

Strukturmechanik, DE 

New Cooperation Methods 

between Industry and 

Academia: The Research 

Training Group 

(Graduiertenkolleg) - Aspects 

of Future Satellite 

Reconnaissance Missions - 

S. Fasoulas¹; K. Janschek¹; K. 

Schönherr²; G. Willich²; A. 

Weber¹; 

¹TU Dresden, DE; ²EADS 

Astrium GmbH, DE 

ECC Room 2 

Numerical Validation of 

Unsteady Transonic Blade 

Row Interaction in a 1½ Stage 

HP Turbine 

J. Dähnert, Technical University 

Berlin, DE; L. Willer, Rolls- 

Royce Deutschland, DE 

ECC Room 3 

Overview of the Soyuz at CSG 

Programme 

H. Arend¹; J.M. Astorg, CNES, 

FR; B. Gerard, Arianespace, FR; 

D. Coulon¹; D. Crowther¹; J. 

Donadel¹; E. Lefort¹; J. Pascual¹; 

N. Pottier¹; 

¹ESA, FR 

ECC Room 1 

15 

11:20 – 11:40 11:40 – 12:00 12:00 – 12:20 12:20 – 12:40 

Space Propulsion I 

Chair: O. Haidn, DLR Lampoldshausen, DE 

An Experimental Study on the 

Base Flow Plume Interaction of 

Booster Configurations 

A. Henckels¹; A. Gülhan¹; D. 

Neeb, RWTH Aachen, DE; 

¹DLR, DE 

Launcher Technologies I 

Chair: TBD 

Enabling Technologies for the 

Next Generation Reignitable 

Cryogenic Upper Stage 

M. Müller; J. Krüger; EADS 

Astrium, DE 

Young Professional Conference II 

Chair: TBD 

Experimental Investigation of 

Coking Characteristics of 

Kerosene Jet A-1 with Respect 

to Practical Applications 

J. Meinert, TU Dresden, Institute 

of Thermodynamics and Building 

Energy Syst, DE 

PRORA-USV: the First 

Dropped Transonic Flight Test 

G. Russo, CIRA, IT 

Comparison between Real and 

Ideal Sub and Supercritical 

Combustion Simulations for 

LO2-CH4 LRE at 15MPa 

A. Minotti; C. Bruno; University of 

Rome La Sapienza, IT 

Trends in the Use of Solid 

Rocket Motors and Effects on 

the Space Debris Environment 

S. Stabroth¹; M. Oswald¹; C. 

Wiedemann¹; H. Krag²; H. 

Klinkrad²; P. Vörsmann¹; 

¹Institute of Aerospace Systems, 

TU Braunschweig, DE; ²Space 

Debris Office, ESA/ESOC, DE 

ECC Room 2 

Preliminary Characterisation 

of Solar Sailing Materials 

C.O.A. Semprimoschnig; A.W. 

Polsak; S. Heltzel; M. Gaud; 

ESA, NL 

ECC Room 3 

TICTAC - Technology of Insert 

Conductive Thermally and 

Attenuator of Shock 

S. Laborde, EADS ASTRIUM, 

FR; L. Mallet, SMAC, FR; R. 

Redondo, CNES, FR 

ECC Room 1


08:30- 

09:30 


09:40 – 10:00 10:00 – 10:20 10:20 – 10:40 10:40 – 11:00 

Korean Session 

Chair: TBD 

Development and Simulation 

of Nonlinear Aeroelastic 

Analysis System for Advanced 

Transonic Aircrafts 

I. Lee; J.-Y. Kim; K.-S. Kim; 

Korean Society for Aeronautical 

and Space Sciences, KR 

Structures: Turbo Machines 

Chair: C. Galinski, PL 

Damping of a Compressor 

Vane Cluster 

A. Hartung; U. Retze; MTU Aero 

Engines, DE 

History 

Chair: W. Heinzerling, DE 

Historical Review and Analysis 

of Santos Dumonts 14-Bis 

F.M. Catalano; P.S. Greco; 

Aerodynamic Laboratory - 

University of Sao Paulo, BR 

Satellite Development Status 

of Korea 

J.-J. Lee; I.-M. Jin; S.-W. Rhee; 

Y.-S. Kim; Korea Aerospace 

Research Institute, KR 

Advanced Coatings for 

Rotating Aero Engine 

Components 

M. Peters¹; U. Schulz¹; B. 

Saruhan-Brings¹; M. Fröhlich¹; R. 

Braun¹; A. Flores Renteria²; C. 

Leyens²; 

¹DLR, DE; ²Technical University 

of Brandenburg, DE 

Albatros- und Heinkel- 

Flugzeuge bei der 

Fliegerschule der Reichswehr 

in Lipezk 

P. Korrell, DE 

Introduction of Korean 

Aerospace Industry and T-50 

Advanced Trainer 

A. Jun, Korean Aerospace 

Industry, KR 

Influence of Air Flow on Blisk 

Vibration Behavior 

B. Beirow; A. Kühhorn; S. 

Schrape; BTU Cottbus, DE 

Sind die Flügel von Raffaels 

Amor in seiner Freske - Die 

drei Grazien - hochgeschwindigkeitstauglich? 

H.-U. Meier, TU Clausthal, DE 

Room Paris 

Supersonic Combustion in 

Ram Accelerator and Scramjet 

Engine Combustor 

I.-S. Jeung; J.-Y. Choi; Seoul 

National University, KR 

Estrelsaal A 

Filament Winding Technology 

- Example of an Integral 

Engine Nose Cone 

O. Lenk¹; M. Dieling¹; R. 

Grothaus, East4D Lightweight 

Structures, DE; 

¹Rolls-Royce Deutschland, DE 

ECC Room 4 

Statistical Investigations 

about Pioneers of Rocketry 

and Space Travel 

D.B. Herrmann, ASTW, DE 

16 

11:20 – 11:40 11:40 – 12:00 12:00 – 12:20 12:20 – 12:40 

Advanced Aero-Engine Concepts 

Chair: I. Dubois, Snecma, FR 

Toward ACARE 2020: 

Innovative Engine 

Architectures to Achieve the 

Environmental Goals? 

S. Dron, Snecma, FR 

The Geared Turbofan 

Technology - Opportunities, 

Challenges and Readiness 

Status 

C. Riegler; C. Bichlmaier; MTU 

Aero Engines, DE 

Structures - CF Manufacturing 

Chair: J.F.M. Wiggenraad, National Aerospace Laboratory NLR, NL 

New Fibre Reinforced 

Ceramics - A Technology 

Driver for New Products 

H. Voggenreiter; B. Heidenreich; 

J. Göring; German Aerospace 

Center (DLR), DE 

Aerospace communications 

Chair: T. Wittig, Euro Telematik, DE 

Broadband Communications 

for Aeronautical Networks: The 

ATENAA Outer Optical Link 

Validation 

C. Fuchs¹; H. Henniger¹; B. 

Epple¹; D. Giggenbach¹; M. 

Amirfeiz²; M. Jentile²; G. Di Nepi²; 

G. Martini³; F. Mazzi³; 

¹German Aerospace Center 

(DLR), DE; ²Selex 

Communications, IT; ³INSIS 

S.p.A., IT 

Innovative Manufacture of 

Aerospace Structural 

Composites Applying the out 

of Autoclave Quickstep 

Process 

C. Weimer, Eurocopter 

Deutschland, DE; M. Kaiser¹; C. 

Garschke²; B. Fox²; K. 

Drechsler¹; 

¹Institut für Flugzeugbau - 

Universität Stuttgart, DE; ²Deakin 

University Geelong, AU 

A Comparison of Estimation 

Methods for the VHF Voice 

Radio Channel 

M. Gruber, Eurocontrol 

Experimental Centre, AT; K. 

Hofbauer, Graz University of 

Technology, AT 

Active Core Technology within 

the NEWAC Research Program 

for Cleaner and More Efficient 

Aero Engines 

S. Bock; J. Sieber; G. Wilfert; 

MTU Aero Engines, DE 

Elektromagnetisch 

Unterstützte Fertigung von 

Faserverbundkunststoffen 

M.P. Podkorytov; T. Stroehlein; 

Deutsches Zentrum für Luft- und 

Raumfahrt e.V., DE 

The SANTANA Project 

A.F. Jacob, Institut für 

Hochfrequenztechnik/ 

Technische Universität Hamburg, 

DE; S. Holzwarth, IMST GmbH, 

DE; A. Dreher, DLR, DE; C. 

Hunscher, EADS Astrium GmbH, 

DE 

Room Paris 

Nacelle Lines for Small Next 

Generation Engines 

R. Schweikhard; J.A. Lieser; 

Rolls-Royce Deutschland, DE 

Estrelsaal A 

Combineded Prepreg and 

Infusion Technology 

R. Kaps; L. Herbeck; German 

Aerospace Center, DE 

ECC Room 4 

B-AMC - Aeronautical 

Broadband Communication in 

the L Band 

C.H. Rokitansky¹; M. Ehammer¹; 

T. Gräupl¹; S. Brandes²; S. 

Gligorevic²; M. Schnell²; C. 

Rihacek³; M. Sajatovic³; 

¹University of Salzburg, AT; 

²German Aerospace Center 

(DLR), DE; ³Frequentis GmbH, 

AT


08:30- 

09:30 


09:40 – 10:00 10:00 – 10:20 10:20 – 10:40 10:40 – 11:00 

Mechanical Architecture, Design and Engineering 1 

Chair: H. Baier, TU München, DE 

Deployment Analysis of Solar 

Arrays and Model Correlation 

A. Carpine; G. Laduree; Thales 

Alenia Space, FR 

Random Vibration and Acoustics 1 

Chair: N. Wijker, Airbus Deutschland, DE 

Vibroacoustic Study of Corot: 

Analysis and Test Correlation 

R. Redondo; A. Pradines; CNES, 

FR 

Short Course 1 

Chair: TBD 

The Influence of Load and 

Deformation on the Fracture 

Behavior of Specimens and 

Structures 

G. Schullerer; M. Windisch; MT 

Aerospace AG, DE 

Vibro-Acoustic Response 

Analysis of the Planck Internal 

Solar Array Panel Applying 

Boundary Element Analysis 

P. di Francescantonio, STS, IT; 

J. Wijker, Dutch Space BV, NL 

Functional Membranes - a 

Basis for Satellite 

Architectures of the Future 

H.J. Baier; L. Datshvili; S. Rapp; 

TU Muenchen, DE 

Simulation of a Spacecraft 

Acoustic Test by Hybrid 

FEM/SEA Method: Application 

to the CALIPSO Spacecraft and 

Comparison with Experimental 

Data. 

R. Knockaert, Alcatel Alenia 

Space, FR; S. Frikha, ESI Group, 

FR 

Estrelsaal C1 

Efficient Mechanism 

Simulation for Solar Array 

Deployment Analysis 

B. Specht, EADS ASTRIUM, DE 

Estrelsaal C3 

Herschel SVM STM Vibro- 

Acoustic Test / Prediction 

Comparison 

L. Trittoni; P.C. Marucchi- 

Chierro; Alcatel Alenia Space - 

Italy, IT 

ECC Room 5 

11:20 – 11:40 11:40 – 12:00 12:00 – 12:20 12:20 – 12:40 

Inflatable / Deployable Structures 1 

Chair: J. Block, DLR Braunschweig, DE 

Slotted Thin Shell Deployable 

Reflector Antennas 

L.T. Tan; S. Norager; University 

College London, GB 

Random Vibration and Acoustics 2 

Chair: M. Link, Universität Kassel, DE 

Introduction of JAXA Tool for 

Random Vibrations Prediction 

and Its Recent Upgrading 

Q. Shi; S. Ando; M. Tsuchihashi; 

JAXA, JP 


Chair: TBD 

Self-deployed Structures and 

Polymer Material with Shape 

Memory 

G.A. Pavlov, IPCP RAS, RU 

Vibration Response of 

Spacecraft under Fill Effect 

S. Ando; Q. Shi; K. Nagahama; 

M. Tsuchihashi; Japan 

Aerospace Exploration Agency 

(JAXA), JP 

Short Course Aircraft Design 

Details will be published on www.ceas2007.org 

17 

The Innovative Deorbiting 

Aerobrake System IDEAS: the 

Gossamer Technology for 

Micro-satellite Deorbiting 

B. Santerre¹; O. Le Couls¹; C. 

Dupuy, CNES, FR; 

¹EADS Astrium, FR 

Level Homogenity versus 

Frequency in a Reverberant 

Chamber 

A. Girard; E. Cavro; Intespace, 

FR 

Estrelsaal C1 

Pressure Restraint Design for 

Inflatable Space Habitats 

M.L. de Jong, Thin Red Line 

Aerospace Ltd., CA; A.B. 

Andrew Lennon, ABL 

Engineering Ltd., IE 

Estrelsaal C3 

Insights into the Equipment 

Random Vibration 

Environment based on 

Simulations of an Acoustic 

Test Bench 

B.J. Brevart, Thales Alenia 

Space, FR; A. Pradines, CNES, 

FR 

ECC Room 5


14:00- 

15:00 

Airbus A380 Forum 

15:10 – 15:30 15:30 – 15:50 15:50 – 16:10 16:10 – 16:30 

Air Transport and Environment 

Chair: J. König, Airbus Deutschland, DE 

Aviation and Climate Change: 

A Comparison of the 

Overflights of the Belgian 

Territory and the Local 

Aviation Activities 

L.E. Matheys¹; T. Festraets²; A. 

Ferrone, Université Catholique 

de Louvain - ASTR, BE; J. Van 

Mierlo¹; C. Macharis²; 

¹Vrije Universiteit Brussel - 

ETEC, BE; ²Vrije Universiteit 

Brussel - MOSI-T, BE 

The Variability of Air 

Transports Specific CO2 

Emissions and its Implications 

for Airline Strategies 

M. R. Schaefer; W. Grimme; 

German Aerospace Center 

(DLR), DE 

Air Data and Navigation Sensor Systems 

Chair: H. von Viebahn, Diehl Aerospace, DE 

A Precision, Time-Relative 

GPS Approach for Measuring 

Kinematic Trajectories Using 

Miniaturized L1 GPS Receivers 

J.P. Traugott¹; O. Montenbruck, 

DLR, DE; G. Sachs¹; 

¹ Technische Universität 

München, DE 

Design and Implementation of 

an Integrated Wind-/Airdata- 

and Navigation System Based 

on Low-Cost Sensor 

Components 

S. Myschik, IABG mbh, DE; G. 

Sachs, Technische Universität 

München, DE 

Numerical Simulation 

Chair: C. Rossow, DLR Braunschweig, DE 

Future Simulation Concept 

J. Klenner, Airbus SAS, FR 

Future Simulation Technology 

Centers in Europe 

K. Becker, Airbus Deutschland, 

DE 

Investigations of Atmospheric 

Conditions Influence on Sonic 

Boom 

S. Chernyshev; A.P. Kiselev; 

P.P. Vorotnikov; TSAGI, RU 

Angles of Attack and Sideslip 

Reconstruction Using Neural 

Networks 

V. Poggi; A Calia; F Schettini; 

University of Pisa, IT 

Future Design Concept 

M. Cross; M. Aston; Airbus, GB 

ECC Hall C 

Reinhardt Abraham - Lufthansa 

Stiftungspreis für die 

Studienarbeit zum Thema: 

Entwurf eines 

Simulationsmodells zur 

Ermittlung des 

wirtschaftlichen Potentials 

von Fluglärmreduzierungsmaßnahmen 

E. Anton, RWTH Aachen, DE 

ECC Hall D 

Zeppelin-Stiftungspreis der 

Stadt Friedrichshafen für die 

Diplomarbeit zum Thema: 

Development of a 

Microcontroller Based Sensor 

Aquisition System for 

Uninhabited Aerial Vehicles 

D. Höse, UniBw München, DE 

Estrelsaal B 

Challenges for Development 

of Numerical Simulation 

N. Kroll, Airbus Deutschland, DE 

18 

16:50 – 17:10 17:10 – 17:30 17:30 – 17:50 17:50 – 18:10 

SESAR 

Chair: T. Mühlhausen, DLR Braunschweig, DE 

The Concept of Operations for 

the Future European Air Traffic 

Management System being 

Defined by SESAR 

J. R. F. Guy, Air Traffic Alliance, 

FR 

Flow Simulation and Validation 

Chair: T. Schönfeld, CERFACS, FR 

QNET-CFD Knowledge-Base - 

A Platform for the Preservation 

of Knowledge Generated by EU 

Funded Projects 

J.B. Vos, CFS Engineering, CH; 

A,G. Hutton, Qinetic, GB; C. 

Hirsch, NUMECA, BE 

An Airports View on the 

SESAR Operational Concept 

M. Huhnold, Fraport AG, DE 

Reynolds Number Effects on 

Blunt Leading Edge Delta 

Wings 

S. Crippa; A. Rizzi; KTH, Dept. of 

Aeronautical and Vehicle 

Engineering, SE 

Flight Control - Functions and Control Laws 

Chair: S. Levedag, DLR Braunschweig, DE 

Nonlinear Flight-Path Control - 

A Flight Dynamics Perspective 

F. Holzapfel, IABG mbH, DE; L. 

Höcht¹; F. Schuck¹; G. Sachs¹; 

¹Lehrstuhl für Flugmechanik und 

Flugregelung, TU München, DE 

Advanced Gust Load 

Alleviation System for Large 

Flexible Aircraft 

S.L. Hecker; K.-U. Klaus-Uwe 

Hahn; DLR, DE 

DFS Deutsche Flugsicherung 

GmbH Aligning their Research 

& Development Needs for the 

Single European Sky Air 

Traffic Management Research 

Programme (SESAR) 

T. Bierwagen, DFS Deutsche 

Flugsicherung GmbH, DE 

Inlet Boundary Conditions for 

Embedded LES 

L.J. Davidson, Chalmers 

University of Technology, SE 

Direct Force Control Using 

Brake Flaps for Improving 

Flight Path Control 

G. Sachs, Institute of Flight 

Mechanics and Flight Control of 

TU München, DE 

ECC Hall C 

European Research Center 

Position and Contribution in 

European R&D for Single 

European Sky Air Traffic 

Management Research 

Programme (SESAR) 

K.-H. Keller, German Aerospace 


ECC Hall D 

CFD Validation of Unsteady 

Installed Propeller Flows 

Using the DLR TAU-Code 

A. Stuermer, DLR, DE 

Estrelsaal B 

Aircrafts Control Systems 

Design: An H_infinity Loop- 

Shaping Approach 

R. Panesi; G. Mengali; 

University of Pisa, IT


14:00- 

15:00 


15:10 – 15:30 15:30 – 15:50 15:50 – 16:10 16:10 – 16:30 

Aerodynamics 1 

Chair: TBD 

Further Investigation on Vortex 

Turbulent Characteristics in 

Pattern Transition of a SFRJ 

Simulator 

S.C. Lee, Yung Ta, Institute of 

Technology and Commerce, TW 

Planetary Exploration 

Chair: TBD 

The Radio Science Experiment 

“VeRa” onboard ESA´s Venus 

Express Spacecraft 

R. Mattei, Institut für Raumfahrttechnik, 

UniBw, DE; B. Häusler¹; 

M. Pätzold²; S. Remus, VEGA, DE; 

W. Eidel¹; S. Tellmann²; T. Andert¹; 

J. Selle¹; M.K. Bird, Argelander - 

Institut für Astronomie, Universität 

Bonn, DE; R.H. Simpson³; G.L. 

Tylor³; 

¹Institut für Raumfahrttechnik, 

UniBw, DE; ²Rheinisches Institut für 

Umweltforschung, Universität Köln, 

DE; ³Department of Electrical 

Engineering, Stanford University, 

US 

Young Professional Conference III 

Chair: TBD 

Active flow Control on the 

Simplified Flapped Airfoil 

M. Matejka¹; N. Souckova¹; L. 

Popelka, Academy of Science of 

the Czech Republic, Institute of 

Thermomechanics, CZ; J. 

Nozicka¹; 

¹CTU in Prague, FME, CZ 

The Stuttgart Moon Orbiter 

LUNAR MISSION BW1 

R. Laufer; H.-P. Roeser; - Lunar 

Mission BW1 Project Team; 

Institute of Space Systems (IRS), 

Universitaet Stuttgart, DE 

Numerical Investigation of 

Upstream Moving Wave 

Phenomenon in Unsteady 

Transonic Airfoil Flow 

V. Hermes, 

ShockWaveLaboratory/RWTH- 

Aachen University, DE; I. 

Klioutchnikov¹; A. Alshabu¹; H. 

Olivier¹; 

¹ShockWaveLaboratory, DE 

Regenerative Fuel Cells for 

Mars Missions 

M. Hörenz; S. Fasoulas; T. 

Schmiel; K. Zajac; TU Dresden, 

DE 

ECC Room 2 

Steady Longitudinal Vortices 

in Separated Turbulent Flows 

E. Schülein, DLR, DE; V. 

Trofimov, NSPU, RU 

ECC Room 3 

Probenpräparation, 

Probenhandling und 

Nutzlastaspekte für die 

Europäische ExoMars Mission 

P.H. Hofmann, Kayser-Threde 

GmbH, DE 

ECC Room 1 

19 

16:50 – 17:10 17:10 – 17:30 17:30 – 17:50 17:50 – 18:10 

Optimisation of Aerodynamic Aircraft Configurations 

Chair: TBD 

Towards Aerodynamic Design 

by Optimisation of Transonic 

Transport Aircraft in an Multi- 

Disciplinary Environment 

G. Carrier; S. Mouton; M. 

Marcelet; C. Blondeau; ONERA, 

FR 

New Space Missions 

Chair: P. Hofmann, Kayser-Threde, DE 

Lunar Infrastructure for 

Exploration - European 

Roadmap and Reference 

Concept 

H.-J. Heidmann, Astrium ST, DE 

Young Professional Conference IV 

Chair: TBD 

Multi-objective Optimisation of 

Aircraft Range and Fuel 

Consumption 

W.J. Vankan; M. Laban; E. 

Kesseler; NLR, NL 

A Scientific and Technological 

Lunar Lander Mission 

D. Wilde; P. Kyr; Astrium ST, DE 

VEGA RACS Waterhammer 

Analysis 

F.J. Dengra; M. Gralher; B. 

Behrens; Astrium ST, DE 

KAP - An In-Orbit Test Facility 

for Technology Demonstration 

and Scientific Use 

C. Kaiser¹; G. Pont¹; A. Conde 

Reis, ESTEC/ESA, NL; 

¹Kayser-Threde GmbH, DE 

ECC Room 2 

Next Generation Missile 

Aerodynamic Visualisation 

with CFD 

K. Weinand; D. Stern; MBDA 

LFK, DE 

ECC Room 3 

Time Resolved Measurement 

of Atomic Oxygen in Low 

Earth Orbit and its Benefits 

for Future Spacecraft Design 

T. Schmiel; S. Fasoulas; J. 

Heisig; O. Przybilski; TU 

Dresden, DE 

ECC Room 1


14:00- 

15:00 


15:10 – 15:30 15:30 – 15:50 15:50 – 16:10 16:10 – 16:30 

Environment and noise 

Chair: M. Pfitzner, UniBw München, DE 

On the Development of 

Combustion Systems and their 

Design Methodologies for the 

Reduction of Pollutant 

Emissions from Aero-Engines - 

The European Project 

INTELLECT D.M. 

R. von der Bank, Rolls-Royce 

Deutschland, DE; N. Savary, 

Turbomeca, FR; M. Alden, Lunds 

Universitet, SE; M. Zedda, Rolls- 

Royce, GB; J. McGuirk, 

Loughborough University, GB; G. 

Cinque, AVIO, IT 

Structures - CF Application 

Chair: TBD 

Walther Blohm-Studienpreis für 

die Studienarbeit zum Thema: 

Vergleichende Analyse der 

konzentrierten 

Einzelkrafteinleitung in eine 

Rechteckscheibe mittels 

kontinuumsmechanischer und 

FEM-Berechnung sowie 

Experiment 

R. Basan, TU Berlin, DE 

Strategy for Environmentally 

Friendly Low Emissions 

Combustion Development in 

European Aeronautics 

R. von der Bank, Rolls-Royce 

Deutschland, DE; M. Cazalens, 

SNECMA, FR; C. Berat, 

Turbomeca, FR; S. Harding, 

Rolls-Royce, GB 

Experimentelle 

Untersuchungen zum 

Biegeeinfluss an Flachproben 

mit Nähten unterschiedlicher 

Parameter unter Einsatz von 

optischen Messverfahren 

F. Kruse; H.-G. Reimerdes; 

RWTH Aachen, DE 

Aerospace Information Technologies and Electronics 

Chair: P. Stütz, ESG Elektroniksystem- und Logistik-GmbH, DE 

Challenges for IT Infrastructure 

Supporting Secure Network- 

Enabled Commercial Airplane 

Operations 

R.V. Robinson¹; R. Krishna 

Sampigetha¹; M. Li¹; S.A. 

Lintelman¹; D. von Oheimb, 

Siemens, DE; R. Poovendran, 

University of Washington, US; 

¹Boeing, US 

Software: The Underestimated 

Component in Space Missions 

S. Montenegro, Fraunhofer 

Institut FIRST, DE 

Influence of the Bypass Ratio 

on Low Altitude NOx 

Emissions 

H. Hemmer; T. Otten; M. Plohr; 

M. Lecht; A. Döpelheuer; DLR, 

DE 

Ludwig Bölkow-Stiftungspreis für 

die Diplomarbeit zum Thema: 

Untersuchung der Interaktion 

benachbarter Schichten bei 

schwingender Beanspruchung 

von Faser-Kunststoff- 

Verbunden 

T. Hensel, TU Darmstadt, DE 

Topological Design of a High 

Altitude Platform using a 

System Design Language 

M. A. Haq, TAO-Technologies 

GmbH, DE; B. Kröplin, Institute 

for Statics and Dynamics of 

Aerospace Structures, DE 

Room Paris 

Noise Radiation through Aero- 

Engine Exhausts - Large 

Scale Model Experiments 

F. Arnold, Rolls-Royce 

Deutschland, DE; U. Tapken, 

DLR, DE; J. Zillmann, EADS 

Corporate Research Center, DE 

Estrelsaal A 

Willy Messerschmitt-Preis für die 


Deformation Fields Estimation 

Using Fibre Bragg Gratings 

St. Rapp, TU München, DE 

ECC Room 4 

Extension of EDA Toolbox for 

VHF Data Link System 

Simulation 

H. Flühr, FH JOANNEUM Graz, 

AT 

20 

16:50 – 17:10 17:10 – 17:30 17:30 – 17:50 17:50 – 18:10 

Aero-Engine Components: Turbines / Combustors 

Chair: H. Knittel, MTU Aero Engines, DE 

Preparation of Aero 

Technology for New 

Generation Aircraft Engine LP 

Turbines 

J. Gier; T. Schröder; I. Raab; 

MTU Aero Engines, DE 

Structures - Miscellaneous 

Chair: A. Viviani, IT 

The Delamination Behaviour of 

Carbon Composite Structures 

Manufactured with the Vacuum 

Assisted Process (VAP) 

G. Spenninger, EADS Military Air 

Systems, DE; H. Bansemir¹; M. 

Schulz¹; 

¹Eurocopter Deutschland GmbH, 

DE 

Space Control and Simulation 

Chair: M. Bandecchi, ESA/ESTEC, NL 

Calibration of the Micro- 

Newton Propulsion System for 

the LISA Pathfinder Drag-Free 

Satellite 

T. Ziegler¹; M. Göbel²; A. 

Schleicher¹; W. Fichter²; 

¹EADS Astrium GmbH, DE; 

²University of Stuttgart, DE 

Numerical Modeling of 

Aviation Gas Turbine Cooled 

Elements 

A. Sadiqov; A. Pashayev; D. 

Askerov; A. Samedov; R. 

Mamedov; National Academy of 

Aviation, AZ 

Numerical Simulation of 

Advanced Folded Core 

Materials for Structural 

Sandwich Applications 

S. Heimbs¹; P. Middendorf¹; S. 

Kilchert²; A.F. Johnson²; M. 

Maier, Institute for Composite 

Materials (IVW), DE; 

¹EADS Innovation Works, DE; 

²German Aerospace Center 

(DLR), DE 

Orbital Maneuvering of the 

VEGA Launcher 

G. Martens; P. Bini; I. Cruciani; 

C.R. Roux; ELV, IT 

Passive Shroud Cooling 

Concepts for HP Turbine 

Blades 

E. Janke, Rolls-Royce 


Finite Elemente Simulation 

einer Notwasserung eines 

Transportflugzeugs zur 

Ermittlung der dabei 

auftretenden Lasten 

T. Schmid-Fuertes; R. Curtius; J. 

Mendler; EADS Military Air 

Systems, DE 

Flight Software Driven Rigid 

Body - Computational Fluid 

Dynamics Closed Loop 

Simulation 

M.I. Panevsky; B.J. Pataky; P.T. 

Than; The Aerospace 

Corporation, US 

Room Paris 

Parametric Study of Soot 

Formation in an Aeroengine 

Model Combustor at Elevated 

Pressures by Laser-Induced 

Incandescence: Effect of the 

Fuel Phase 

U.E. Meier¹; C. Hassa¹; K.P. 

Geigle²; O. Lammel²; P. Kutne²; 

¹DLR Inst. of Propulsion 

Technology, DE; ²DLR Inst. of 

Combustion Technology, DE 

Estrelsaal A 

EMI Control in the Presence of 

Composite Materials 

F. Thurecht¹; M. Leininger, 

Kayser-Threde GmbH, DE; C. 

Schöppinger, INVENT GmbH, 

DE; L. Trougnou, ESA-ESTEC, 

NL; E. Pfeiffer¹; 

¹HPS GmbH, DE 

ECC Room 4 

Analytical Approach for the 

Solution of Super-/ 

Hypersonic Flow Fields 

B. Thorwald; C. Mundt; 

Universität der Bundeswehr, 

München, DE


14:00- 

15:00 


15:10 – 15:30 15:30 – 15:50 15:50 – 16:10 16:10 – 16:30 


Chair: S. Langlois, European Space Agency, ESA/ESTEC, NL 

Large Deployable Membrane 

Structures 

M. Straubel¹; C. Sickinger¹; S. 

Langlois, ESA/ESTEC, NL; 

¹DLR - Institut für 

Faserverbundleichtbau und 

Adaptronik, DE 

Bending-Wrinkling 

Characteristics of the Inflated 

Boom 

H. Tan¹; C. Wang¹; J. Yang, 

China Academe of Space 

Technology, CN; X. Du¹; H. Tan¹; 

¹Harbin Institute of Technology, 

CN 

Shock 1 

Chair: A. Capitaine, Astrium EADS SAS, FR 

Statistical Processing of Shock 

Test Data 

G. LADUREE, Thales Alenia 

Space, FR; S. KIRYENKO, ESA, 

NL 


Chair: TBD 

Herschel SVM Shock 

Qualification Test / Prediction 

Comparison - An Industrial 

Experience 

P.C. Marucchi-Chierro, Thales 

Alenia Space, IT 

The Application of Shape 

Memory Polymer Composite to 

Deployable Hinge for Solar 

Arrays 

J. Leng, Harbin Institute of 

Technology, CN 

Main Outcomes of CNES 

Launcher Directorate Research 

Group on Shock Propagation 

into Launcher Structures 

P. Roux, CNES, FR 

Estrelsaal C1 

Design and Analysis of Full- 

Scale Stiffened-Spring Back 

Reflector 

O. Soykasap, Afyon Kocatepe 

University, TR; L.T. Tan, 

University College London, GB 

Estrelsaal C3 

Reliability Demonstration of 

the Pyrosoft Release Nut 

P. Thebault, Etienne LACROIX 

Tous Artifices S.A., FR 

ECC Room 5 

16:50 – 17:10 17:10 – 17:30 17:30 – 17:50 17:50 – 18:10 


Chair: T. Henriksen, European Space Agency, ESA/ESTEC, NL 

Failure Testing and Test 

Simulation of the ARIANE 5 

EPC-BME Actuator Brackets 

J. Hoogendoorn; J.F. Koorevaar; 

Dutch Space, NL 

Finite Element Based Initial 

Post-buckling Analysis of 

Conical Shell Structures 

T. Rahman; E.L. Eelco Jansen; 

Delft University of Technology, 

NL 

Shock 2 

Chair: P. Camarasa, EADS-ASTRIUM, FR 

Shock Inputs Derivation to 

Subsystems 

G. Ladurée, Thales Alenia 

Space, FR; J.B. Bernaudin, 

EADS Astrium, FR; S. Kiryenko, 

ESA, NL; S. Mary, CNES, FR 


Chair: TBD 

Shock Propagation in 

Spacecraft Structure 

J.B. Bernaudin¹; E. Courau²; S. 

Mary²; J.B. Verniaud¹; 

¹EADS Astrium, FR; ²CNES, FR 


Details will bepublished on www.ceas2007.org 

21 

Testing of Flexible 

Cu(In,Ga)Se2 Solar Cells for 

Space Applications 

K. Zajac¹; S. Brunner, HTS 

GmbH, DE; K. Otte, Solarion AG, 

DE; S. Fasoulas¹; 

¹Technische Universität Dresden, 

DE 

Qualification to Shock 

Environment in VEGA 

Program, by Full Scale Tests, 

Models and Similarity 

R. Manchini; M. Fragnito; ELV 

SpA Mechanical System 

Development, IT 

Estrelsaal C1 

Reliability of Shell Structures 

Through Sensitivity Analysis 

M.B. Oberguggenberger; B. 

Schmelzer; J. King; Universität 

Innsbruck, AT 

Estrelsaal C3 

HSS3-An Improved Concept 

for the Horizontal Separation 

System of the Ariane5 

Payload Fairing and its 

Qualification Status 

P.R. Bodagala, CNES, FR; M. 

Rendina, Oerlikon Space, CH 

ECC Room 5

Wednesday, 12th September 2007 

08:30- 

09:30 

ATM Forum 

09:40 – 10:00 10:00 – 10:20 10:20 – 10:40 10:40 – 11:00 

Wake Vortex Advisory Systems 

Chair: T. Rötger, Airbus Deutschland, DE 

Wake Vortex Advisory 

Systems USA, SOIA 

S.R.L. Lang¹; J.A. Tittsworth¹; 

W.H. Bryant, NASA, US; J.P. 

Nicolaon, National Institute for 

Aerospace, US; 

¹Federal Aviation Administration, 

US 

Unmanned Aircraft Systems 

Chair: C. Le Tallec, Onera, FR 

A Solar Powered HALE-UAV 

for Arctic Research 

H. Runge¹; W. Rack, University 

of Canterbury, NZ; A. Ruiz-Leon¹; 

M. Hepperle¹; M. Hanke¹; D. 

Holzhüter¹; 

¹DLR, DE 

Wake Turbulence Mitigation for 

Departures from Closely 

Spaced Parallel Runways: A 

Research Update 

J.A. Tittsworth¹; S.R. Lang¹; D.A. 

Domino²; G. Lohr, NASA, US; 

C.R. Lunsford²; D.A. Clark³; F.M. 

Robasky³; 

¹Federal Aviation Administration, 

US; ²The Mitre Corporation, US; 

³MIT Lincoln Laboratory, US 

Insertion of Unmanned Aircraft 

Systems in Non-Segregated 

Airspace: A Combined 

Technological and Regulatory 

Challenge 

G. Mardiné, SAFRAN-Sagem 

Défense Sécurité, FR 

Flight Control for Missiles 

Chair: K.U. Hahn, DLR Braunschweig, DE 

Case Study: TAURUS 

KEPD350 Integration on 

Tornado Fighter Aircraft 

D. Fasol; H. Neubauer; MBDA 


Comparison of Classical to 

H∞-Norm Optimal Robust 

Autopilot Design 

J.E. Misgeld; A. Reindler; T. 

Kuhn; Diehl BGT Defence, DE 

The Wake Vortex Prediction 

and Monitoring System 

WSVBS - Part I: Design 

F. Holzäpfel¹; T. Gerz¹; M. 

Frech¹; A. Tafferner¹; F. Köpp¹; I. 

Smalikho¹; S. Rahm¹; K.-U. 

Hahn²; C. Schwarz²; W. Gerling²; 

¹DLR-Oberpfaffenhofen, DE; 

²DLR-Braunschweig, DE 

Miniature UAVs Concepts for 

Outdoor Missions 

A. Joulia; S. Bertrand; ONERA, 

FR 

Nonlinear Missile Guidance 

Laws Based on Lyapunov 

Method 

R.T. Yanushevsky, Research & 

Technology Consulting, US 

ECC Hall C 

The Wake Vortex Prediction 

and Monitoring System 

WSVBS - Part II: Performance 

and ATC Integration 

T. Gerz¹; F. Holzäpfel¹; W. 

Gerling¹; A. Scharnweber¹; M. 

Frech, Deutscher Wetterdienst, 

DE; A. Wiegele¹; S. Rahm¹; K. 

Kober¹; 

¹DLR, DE 

ECC Hall D 

Conceptual Design 

Methodology for High Altitude 

Long Endurance UAV 

S. Defoort¹; J. Hermetz¹; N. 

Berend¹; C. Le Tallec¹; R. Bec, 

Cnes, FR; 

¹Onera, FR 

Estrelsaal B 

Multi-spectral Image 

Generation for Real-time 

Hardware-in-the-loop 

Simulations 

R.G. Wiedemann; P. Schätz; 

K.M. Wanie; LFK- 

Lenkflugkoerpersysteme, DE 

22 

11:20 – 11:40 11:40 – 12:00 12:00 – 12:20 12:20 – 12:40 

Wake Vortex R&D 

Chair: A. Reinke, Airbus Deutschland, DE 

Wake Vortex R&D in the USA - 

A Status of Current Progress 

and Plans 

W. H. Bryant, NASA, US; J.P. 

Nicolaon, National Insititute for 

Aeronautics, US; S.L. Lang¹; J.A. 

Tittsworth¹; 

¹FAA, US 

Parametric Study & Simplified 

Approach to Wake Vortex 

Encounter Offline-Simulation 

D. Bieniek, Institute of 

Aeronautics and Astronautics, 

DE 

Air Transport System 

Chair: B. Kiefner, Airbus Deutschland, DE 

EVTS Enhanced VFR Transport 

System 

J. Groeneweg, NLR, NL; R. van 

Gent, TNO, NL; W.R. Berkouwer, 

ASTI, NL 

Level of Service for Aviation 

Infrastructure Markets? 

E. Grunewald, DLR e.V., DE 

Rotorcraft 

Chair: B. Gmelin, DLR Braunschweig, DE 

Helicopter Noise and Vibration 

Reduction with Adaptive Fiber 

Composites 

T. H. Brockmann, Eurocopter 


Structural Design and 

Optimization of the Integrated 

Active Trailing Edge Concept 

for a Helicopter Rotor Blade 

E.A. Ahci¹; R.P. Pfaller¹; A.S. 

Schuld, Bundeswehr, DE; 

¹Eurocopter, DE 

Investigation of Four Vortex 

System Wake Characteristics 

A. Allen; C. Breitsamter; TU 

München, Institute of 

Aerodynamics, DE 

Defining the Future European 

Air Traffic Management 

System for 2020 and Beyond : 

The Vision from SESAR 

S. Reed, Air Traffic Alliance, FR 

Crash Analysis of the “High 

Cabin”-Version of the NH90 

Transport Helicopter Fuselage 

J.O Majamäki, Eurocopter 


ECC Hall C 

A Comparison between CFD 

and Wind Tunnel 

Measurements for Wake 

Vortex Prediction 

S. Melber-Wilkending, DLR 

Braunschweig, DE; A. Allen¹; C. 

Breitsamter¹; 

¹TU München, DE 

ECC Hall D 

Aviation Safety Plans - The 

Total Systems Approach and 

the Way Forward 

F. Böhm; T. Mickler; BMVBS - 

Bundesministerium für Verkehr, 

Bau und Stadtentwicklung, DE 

Estrelsaal B 

Piezoceramic Actuators for 

Morphing Helicopter Rotor 

B.A. Grohmann; C.K. Maucher; 

P. Jänker; EADS Innovation 

Works, DE


08:30- 

09:30 

ATM Forum 

09:40 – 10:00 10:00 – 10:20 10:20 – 10:40 10:40 – 11:00 

Transport aircraft Aerodynamics 

Chair: G.A. Dirks, Airbus S.A.S, FR 

Parametric Effects on Spoiler 

Geometry Assessment with 

Chimera Technique 

X. Bertrand, Airbus SAS, FR 

On the Comparison of Stalling 

Flow-Through Nacelles and 

Powered Inlets at Take-Off 

Conditions 

S. Schulze; C. J. Kähler; R. 

Radespiel; Institute of Fluid 

Mechanics, TU Braunschweig, 

DE 

Space Systems: Spacecraft Technologies 

Chair: TBD 

A Fleet Management System 

for Commercial Spacerafts in 

GEO Using SMART-OLEV 

C. Kaiser, Kayser-Threde GmbH, 

DE; F. Sjöberg, SSC, SE; J.-M. 

Del Cura, Sener, ES; B. 

Eilersten, OSSL, GB 

ZARM-Preis für die Diplomarbeit 

zum Thema: 

LISA Thermal Control Analysis 

in Context of the BayernSat 

Mission 

S. Höfner, TU München, DE 

Aero-Engine Components: Compressors I 

Chair: U. Wenger, Rolls-Royce Deutschland, DE 

Influence of Blade Mistuning 

on Blisk Vibration 

T. Klauke; A. Kühhorn; B. Beirow; 

BTU Cottbus, DE 

The Capability of Influencing 

Secondary Flow in 

Compressor Cascades by 

means of Passive and Active 

Methods 

A. Hergt¹; R. Meyer¹; K. Engel, 

MTU Aero Engines, DE; 

¹DLR, DE 

Computations of Unsteady 

Aerodynamics due to Body 

Motion 

H. Berglind, FOI, SE; L. 

Djayapertapa, Airbus UK, GB; N. 

Ceresola, Alenia, IT; R. Heinrich, 

DLR, DE; S. Leicher, EADS-M, 

DE; N. Caballero Rubiato, INTA, 

ES; B. Prananta, NLR, NL; V. 

Brunet, ONERA, FR 

Simulation of the Attitude 

Behaviour and Available Power 

Profile of the Delfi-C3 

Spacecraft with Application of 

the EuroSim Platform 

F. te Hennepe; B.T.C. 

Zandbergen; R.J. Hamann; Delft 

University of Technology, NL 

A Feature Based Approach to 

High Pressure Compressor 

Pre-Design for Civil Aircraft 

Propulsion Systems 

S. Bretschneider; S. Staudacher; 

Institut für Luftfahrtantriebe (ILA), 

Universität Stuttgart, DE 

ECC Room 2 

Ferdinand Schmetz-Preis für die 


Investigation of Boundary 

Layer Transition for Small 

Reynolds Numbers in Free 

Flight and Wind Tunnel 

Experiments 

B. Kobiela, University Stuttgart, 

DE 

ECC Room 3 

Imaging Radiometer 

METimage for Future 

Operational Earth Observation 

Platforms in Polar Orbits 

A. Pillukat, Jena-Optronik 

GmbH, DE; H.-P. Nothaft, AIM 

GmbH, DE; C. Brüns, DLR, DE 

ECC Room 1 

Der Axialverdichter im 

Flugtriebwerk - gestern, heute 

und morgen 

L.H. Schmidt-Eisenloher; O.E. 

Kosing; Atena Engineering 

GmbH, DE 

23 

11:20 – 11:40 11:40 – 12:00 12:00 – 12:20 12:20 – 12:40 

Advanced Wing Technologies and Flight Testing 

Chair: J. König, Airbus Deutschland, DE 

Requirements and Results of 

Wake Vortex in-flight 

Measurements in AWIATOR 

J. König, Airbus Deutschland, DE 

Forward Looking Clear Air 

Turbulence Measurement with 

the AWIATOR LIDAR Sensor 

N.P. Schmitt¹; W. Rehm¹; T. 

Pistner¹; H. Diehl¹; P. Nave¹; G. 

Jenaro-Rabadan²; P. Mirand²; M. 

Reymond²; 

¹EADS, DE; ²Airbus, FR 

Space Systems: Launcher Technologies II 

Chair: TBD 

Payload Adaptor System of 

High Performances and Low- 

Shock 

M. Lancho; E. Grande; J. Rivas; 

EADS, ES 

Shock Attenuator System for 

Spacecraft and Adaptor 

P. Camarasa, EADS-ASTRIUM, 

FR 

Aero-Engine Components: Compressors II 

Chair: A. Kühhorn, BTU Cottbus, DE 

Multi-objective Blade Design 

Using a Quasi-3d Nondimensional 

Parameterization 

Approach 

A. K. Dutta; P. M. Flassig; D. 

Bestle; Brandenburg University of 

Technology Cottbus (BTU 

Cottbus), DE 

Multi-Objective Compressor 

Blade Optimisation Using a 

Non-Dimensional 

Parameterisation Approach 

P.M. Flassig, BTU Cottbus, LS 

Technische Mechanik und 

Fahrzeugdynamik, DE 

Validation of Low Noise 

Procedures in Simulator and 

Flight Tests 

B. Boche¹; N. Kulwatz, Airbus, 

DE; R. Luckner¹; 

¹TU Berlin, DE 

Payload Adaptor System for 

James Webb Space Telescope 

J. Vilanova; R. Rosa; EADS, ES 

Multi Disciplinary Blading 

Design by Means of Multi 

Objective Optimisation 

D. Otto; D. Bestle; Chair of 

Engineering Mechanics and 

Vehicle Dynamics, BTU, DE 

ECC Room 2 

Results of Large Winglet 

ground and flight testing in 

the European Integrated 

Platform AWIATOR 

N. Wijker, Airbus Deutschland, 

DE 

ECC Room 3 

Shock Attenuation System for 

Spacecraft and Adaptor 

(SASSA) 

M. Lancho; A. Fernandez; 

EADS, ES 

ECC Room 1 

Comparison of different 

Parameterization and 

Optimization Approaches in 

the Field of Aerodynamic 

Compressor Blade Design 

A. Keskin; M. Swoboda; Rolls- 

Royce Deutschland, DE


08:30- 

09:30 

ATM Forum 

09:40 – 10:00 10:00 – 10:20 10:20 – 10:40 10:40 – 11:00 

Air and Space Medicine and Law 

Chair: TBD 

Aircraft Noise Effects on 

Sleep: DLR Research and 

Application to a German 

Airport 

A. Samel; M. Basner; U. 

Isermann; H. Maaß; U. Müller; J. 

Quehl; DLR, DE 

Medical Emergency Area for 

Long-Haul Flights 

J. Heuser, AIDA Development 

GmbH, DE; J. Cremers, Airbus, 

DE 

Supersonic/Hypersonic: Thermal Protection 

Chair: J.M. Longo, DLR Braunschweig, DE 

CIRA-GHIBLI Plasma Wind 

Tunnel: Aerothermodynamic 

Performances Analisys and 

Comparison with the 

SCIROCCO Facility 

P. Carlo¹; F. De Filippis¹; E. 

Graps¹; M. Marini¹; E. 

Bucchignani¹; R. Savino²; S. 

Liberatore²; 

¹CIRA, IT; ²University of Naples, 

IT 

Thermal Qualification of 

Transpiration Cooling for 

Atmospheric Entry 

B. Esser; A. Gülhan; M. Kuhn; 

DLR, DE 

Workshop ICAO for Space 1 

Coordinator: T. Sgobba, ESA/ESTEC, NL 

Noise-Reduced Landing 

Approaches and Pilots 

Workload 

E.-M. Elmenhorst; H. Maaß; M. 

Vejvoda; A. Samel; German 

Aerospace Center (DLR), DE 

In Flight Research on 

Aerothermodynamics (ATD) 

and Thermal Protection 

Systems (TPS) for Space 

Transportation Systems 

J.M. Muylaert; J. Gavira; H. 

Ritter; ESA/ESTEC, NL 

Room Paris 

Perspectives for the Network 

of Centres in the Space 

Domain 

W. Rathgeber, European Space 

Policy Institute (ESPI), AT 

Estrelsaal A 

Aerodynamic Analysis of 

Computed Plate /Jet - 

Interactions for Blunted Cone- 

Cylinders in Hypersonic Flow 

S. Zahir, Computer & IT Centre, 

PK; Z. Ye, Northwestern 

Polytechnical University, CN 

ECC Room 4 

24 

11:20 – 11:40 11:40 – 12:00 12:00 – 12:20 12:20 – 12:40 

UAS: Innovative Concepts 

Chair: W. Engelhardt, MBDA Deutschland, DE 

EADS Technology Activities in 

Communications 

D. Hoffmann, EADS, DE 

Structures - Optimisation 

Chair: H. Hönlinger, DLR Göttingen, DE 

Multidisciplinary, Large Scale 

Optimization of Composite 

Aircraft Structures 

G. Schuhmacher; F. Daoud; J. D. 

Wagner; R. Zotemantel; EADS 

Military Air Systems, DE 

Cost Appreciation of Morphing 

UAV Projects at a Conceptual 

Design Stage. 

T. Melin; A. T. Isikveren; M. I. 

Friswell; University of Bristol, GB 

Structural Optimization of 

Adaptive Airfoils Using 

Evolutionary Algorithms 

J. Seeger; K. Wolf; TU Dresden, 

Institute of Aerospace 

Engineering, DE 

Workshop ICAO for Space 2 

Coordinator: T. Sgobba, ESA/ESTEC, NL 

Motivation der Notwendigkeit 

adaptiver Flugsteuerungen am 

Beispiel der Reglerentwicklung 

für den ARTIS 

Technologiedemonstrator 

S. Lorenz, DLR, DE 

Claudius Dornier Jr.- 

Stiftungspreis für die 


Implementierung eines 

Präprozessors zur Erzeugung 

eines Balkenmodells für die 

multidiziplinäre Optimierung 

G. Wellmer, RWTH Aachen, DE 

Room Paris 

Designing Future Unmanned 

Combat Air Systems From the 

Effector Point of View 

J. Engel, MBDA/LFK, DE 

Estrelsaal A 

GA Optimization of Straight 

and Curved Laminated 

Composites in Presence of a 

Cutout 

A. Gorjipoor, Sharif University of 

Technology, IR 

ECC Room 4


08:30- 

09:30 

ATM Forum 

09:40 – 10:00 10:00 – 10:20 10:20 – 10:40 10:40 – 11:00 

Columbia Accident 

Chair: T. Henriksen, European Space Agency, ESA/ESTEC, NL 

The Space Shuttle Columbia Accident Investigation: Forensic 

Tools, Techniques, and Results 

S. J. McDanels, NASA, US 

Composite Structures 1 

Chair: R. Usinger, Oerlikon Space AG, CH 

Design of Multifunctional 

Folded Core Structures for 

Aerospace Sandwich 

Applications 

Y. Klett, Institut für Flugzeugbau, 

Universität Stuttgart, DE; K. 

Drechsler, Institut für 

Flugzeugbau, Uni Stuttgart, DE; 

M. Kolax¹; H.P. Wentzel¹; R. 

Kehlre, Foldcore GmbH, DE; 

¹Airbus Deutschland GmbH, DE 


Chair: TBD 

Development of Ariane 5 

Vehicle Equipment Bay 

Structure in Fiber Placement 

L. Escudero, EADS - CASA 

Espacio, ES; P. Pablo Lario¹; V. 

Victor Bautista¹; 

¹EADS-CASA Espacio, ES 

Estrelsaal C1 

Space Shuttle Orbiter Columbia Reconstruction and Investigation 

M. Solomon, Boeing, US 

Mechanical and Physical 

Evaluation of a New Carbon 

Fibre/ PEEK Composite 

System for Space Applications 

J.P. Kilroy¹; C.M. Ó Brádaigh¹; 

C.O.A. Semprimoschnig, 

European Space Agency (ESA), 

NL; 

¹Composites Testing Laboratory, 

IE 

Estrelsaal C3 

Compression Strength: The 

Key to Future CFRP 

Production 

C. Arlt; D. Röstermundt; T. 

Mahrholz; U. Riedel; L. Herbeck; 

German Aerospace Centre 

(DLR), DE 

ECC Room 5 

11:20 – 11:40 11:40 – 12:00 12:00 – 12:20 12:20 – 12:40 


Chair: J. Santiago Prowald, European Space Agency, ESA/ESTEC, NL 

Verification Methodology for 

Self-Deploying Support 

Frames 

C. Sickinger; H. Assing; H. 

Koeke; M. Straubel; DLR - 


Mechanical and Environmental 

Validation of a Spherical 

Multipurpose Inflatable 

Structure 

S. Mileti; G. Bitetti; M. Marchetti; 

University of Rome La Sapienza, 

IT 


Chair: A. Obst, European Space Agency, ESA/ESTEC, NL 

Thermo-mechanical 

qualification of Ultra High 

Temperature Ceramic 

structures for space 

application 

R Gardi¹; G. Marino¹; S. Di 

Benedetto¹; M Marini¹; E Trifoni¹; 

R Savino, DIAS (univ. of naples), 

IT; 

¹CIRA scpa, IT 


Chair: TBD 

Increase of Bolted Joint 

Performance by Means of 

Local Laminate Hybridization 

A. Fink, German Aerospace 

Center DLR, DE; P. Camanho, 

INEGI, Instituto de Engenharia 

Mecânica e Gestão Industrial, 

PT; M. Canay, EADS CASA 

Espacio, ES; A. Obst, European 

Space Agency, NL 



25 

Topology Optimization Studies 

for a Contoured Beam 

Deployable Micro-Satellite 

Antenna 

N. Fazli, Sharif Univ. of Tec., IR 

Bioinspired Self-Healing 

Composite Materials for Space 

and Aerospace Applications 

R.S. Trask¹; I.P. Bond¹; C.O.A. 

Semprimoschnig, ESA, NL; 

¹Department of Aerospace 

Engineering, University of Bristol, 

GB 

Estrelsaal C1 

Lessons from Structural 

Design of a Highly-Flexible 

Space Structure: the Space- 

Tow Solar Sail 

B.A. Lennon, ABL Engineering 

Ltd, IE; G. Tibert, KTH (Royal 

Institute of Technology), SE 

Estrelsaal C3 

Composite Fasteners for 

Aerospace Applications 

J.W. de Haan, icotec, CH; M. 

Barbezat, EMPA, CH; A. Obst, 

ESA, NL 

ECC Room 5


14:00- 

15:00 

Objectives of the Bologna Process and effects on aerospace engineer education 

15:10 – 15:50 15:50 – 16:10 16:10 – 16:30 

Poster Session 1 

Details for 

poster session 

please find at 

the end of this 

overview 


Details for 




overview 


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overview 

FLYSAFE 

Chair: K. Burkhardt, Diehl Aerospace, DE 

The European Research Project FLYSAFE: 

Evaluation of Novel Traffic Functionalities for 

Future Airliners 

N. Barraci¹; C. Vernaleken¹; C. Urvoy¹; K. Koch¹; 

A. Andreas, Sindlinger, DE; G. Heidelmeyer¹; U. 

Klingauf¹; 

¹TU Darmstadt, Institut für Flugsysteme und 

Regelungstechnik, DE 

High Lift Aerodynamics 1 

Chair: R. Rudnik, DLR Braunschweig, DE 

An Overview on recent High-Lift Research 

Achievements from Airbus Aerodynamics 

D. Reckzeh; H. Hansen; M. Sutcliffe; K. 

Bohannon; S. Galpin; Airbus, DE 

Aviation Safety 

Chair: K. Burkhardt, Diehl Aerospace, DE 

Parametric Aircraft Trajectory Model for Takeoff 

and Departure 

S. Amelsberg, TU Berlin, DE 

FLYSAFE - Design of the Next Generation 

Integrated Surveillance System 

M. Jirsch, Diehl Aerospace, DE 

ECC Hall C 

ECC Hall D 

CFD Prediction of the Maximum Lift Effects on 

Realistic High Lift Commercial Aircraft 

Configurations within the European Project 

EUROLIFT II 

H. von Geyr; N. Schade; DLR, DE 

Estrelsaal B 

Safety in the Terminal Area - An Approach for a 

Quantitative Assessment 

M. Kietzmann; H. Fricke; Institut für Luftfahrt und 

Logistik, TU Dresden, DE 

26 

16:50 – 17:10 17:10 – 17:30 17:30 – 17:50 17:50 – 18:10 

Operations (Air and Ground) 

Chair: T.M. Cerbe, Fachhochschule Braunschweig/Wolfenbüttel, DE 

Optimised Minima Information 

on Data Driven Aeronautical 

Charts 

T. Grasse; P.R. Wipplinger; T. 

Wiesemann; J. Schiefele; 

Jeppesen GmbH, DE 

High Lift Aerodynamics 2 

Chair: R. Rudnik, DLR Braunschweig, DE 

High Lift Aerodynamics at 

NASA Part 1 

Leavitt; Washburn; Wahls; 

NASA, US 

Highly Efficient Civil Aviation - 

An Opportunity for Present & A 

Vision for Future 

R. Nangia, Nangia Aero 

Research Associates, GB 

High Lift Aerodynamics at 

NASA Part 2 

Leavitt; Washburn; Wahls; 

NASA, US 

Rotorcraft Flight and Structural Dynamics 

Chair: TBD 

EC 135 System Identification 

for Model Following Control 

and Turbulence Modeling 

S.A. Seher-Weiss; W. von 

Gruenhagen; DLR, DE 

Coriolis Force Radial Damper 

Y. Gourinat; J. Morlier; G. 

Michon; IGM - SUPAERO - LMS, 

FR 

The Impact of High Speed 

Intercity Train Access on 

Airport Choice in Germany 

M.C. Gelhausen, German 


Overview of Current 

Achievements and Future 

Challenges for High Lift 

Integration R&T Projects 

S. Bauß; B. Kiefner; Airbus 


Prediction of Rate Limiter 

Effects on Rotorcraft Stability 

P.W. Gollnick, German 

Aerospace Centre, DLR, DE; C. 

Gudrian, Fluidon, DE 

ECC Hall C 

Standardized Concept for 

Passenger Guidance Systems 

at Aerodromes 

M. Schultz; A. Wachtel; H. 

Fricke; TU Dresden, DE 

ECC Hall D 

Validation of in-Tunnel High 

Lift Computations 

T. Delille; J.C. Courty; Dassault- 

Aviation, FR 

Estrelsaal B 

Helicopter Rotor Blade 

Integrated Turbulence 

Detector for Noise and 

Vibration Reduction 

C. Gradolph, DE; T. Ziemann¹; 

G. Müller¹; W.J. Wagner²; V. 

Klöppel²; A. Friedberger¹; J. 

Wilde, University of Freiburg, 

DE; M. Knecht³; C. Breitsamter³; 

¹EADS Innovation Works, DE; 

²Eurocopter Deutschland GmbH, 

DE; ³Technical University of 

Munich, DE


14:00- 

15:00 


15:10 – 15:50 15:50 – 16:10 16:10 – 16:30 


Details for 




overview 


Details for 




overview 


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overview 

Education 1 

Chair: J. Thorbeck, TU-Berlin, DE 

EPMA - European Postgraduate Master in 

Aeronautical Engineering 

D. Scholz, HAW Hamburg, DE 

Space Transportation 1 

Chair: TBD 

Space Transportation Systems - Missions & 

Operations (incl. Ground Infrastructure) 

O. Kalden, Vega IT, DE 

Space Propulsion II 

Chair: O. Haidn, DLR Lampoldshausen, DE 

Challenges of Test Facilities for Space 

Propulsion 

K. Schäfer, DLR, DE 

ECC Room 2 

Education, projects and other aerospace activities 

on Brno University of Technology (Czech Rep.) 

A. Pistek; J. Hlinka; Brno University of Technology, 

Institute of Aerospace Engineering, CZ 

ECC Room 3 

Space Transportation Systems - Propulsion, 

Structures & Subsystems 

R. Lo; H. Adirim; AI: Aerospace Institute, DE 

ECC Room 1 

Multidisciplinary Simulation at the Ariane 5 Nozzle 

Section 

J. Bartolome Calvo; H. Lüdeke; DLR (German 

Aerospace Center), DE 

27 

16:50 – 17:10 17:10 – 17:30 17:30 – 17:50 17:50 – 18:10 

Education 2 

Chair: TBD 

An Implementation of an 

Aircraft Flight Mechanics 

Model for Flight Control Law 

Studies 

L.R.S. Cruz, EMBRAER - 

Empresa Brasileira de 

Aeronautica S.A., BR; K.H. 

Kienitz, ITA (Instituto Tecnologico 

de Aeronautica), BR 

Space Transportation 2 

Chair: TBD 

Space Transportation Systems 

- Projects / Programmatics 

(Development & 

Demonstration) 

R. Pernpeintner, MT-Aerospace 

AG, DE; D. Sygulla, MT 

Aerospace, DE 

IFSys- A TU-Berlin UAV 

Student Project 

A. Hoffmann, TU -Berlin Institute 

of Aeronautics and Astronautics, 

DE 


- Cost (Development, 

Production & Operation) 

D. Koelle, TCS, DE; R. Janovsky, 

OHB-Technology, DE 

Aero-Engine Components: Compressors III 

Chair: A. Kühhorn, BTU Cottbus, DE 

Aerodynamic Technology 

Integration on the TP400 and 

E3E Core Compressors 

H. Gümmer; R. Digele; T. Gietl; 

Rolls-Royce Deutschland Ltd. & 

Co. KG, DE 

Multi Objective Optimization of 

a Fan Blade Using an 

Advanced Parameterization 

Method 

M. N Diaye¹; S. Aubert¹; G. 

Grondin¹; S. Moreau, VALEO, 

FR; P. Ferrand, LMFA, FR; 

¹FLUOREM, FR 

A Strategy for Management 

and Leadership Training for 

the European Defence 

Community 

H. Heumann, CONSULTUM, DE 


- System Concepts & Subsets 

J. Kauffmann, ESA, FR; M. 

Sippel, DLR, DE 

Upgrading of Analytical 

Equations for Adiabatic 

Supersonic Flows 

F. Steinmetz; E. Rosenko; ITLR - 


ECC Room 2 

Information Management vs. 

Education and Training: CIRA, 

Italian Aerospace Research 

Centre, Expertise and Future 

Developments 

F. Diozzi; R. Sannino; CIRA, IT 

ECC Room 3 

Space Transportation 

Systems - Demand / Market 

Analysis 

Ch. Gritzner¹; U. Block¹; M. 

Obersteiner, Astrium Space 

Transportation, DE; 

¹DLR, DE 

ECC Room 1 

Hypersonic Nozzle Flow 

Analysis Using Equilibrium 

Chemistry Model 

I. Mahmood; M.Z. Bashir; S. 

Zahir; NESCOM, PK


14:00- 

15:00 


15:10 – 15:50 15:50 – 16:10 16:10 – 16:30 


Details for 




overview 

Poster Session 8 Launcher 

Chair: TBD 

Details for 




overview 

Development Perspectives for Civil Aviation (Bauhaus Luftfahrt) 

Chair: TBD 

Implication of Ultra High Bypass Engines on 

Aircraft Design Features and Mission 

A. Seitz; S. Donnerhack; J. Seifert; Bauhaus 

Luftfahrt e.V., DE 

History and Lessons Learnt From the 

development of Mechanical Systems for 

Different Launch Vehicles 

V. Gomez Molinero, EADS Casa Espacio, ES 

Climatic Aspects 1 

Chair: TBD 

Room 

Paris 

Perspectives of Vertical / Short Take Off and 

Landing in Commercial Aviation 

C. Gologan; C. Heister; A. Kuhlmann; C. Kelders; J. 

Seifert; Bauhaus Luftfahrt e.V., DE 

Estrelsaal A 

FLACON: Future high-altitude Flight - an attractive 

commercial niche? 

J. Starke, Astrium, DE; J.-P. Belmont, DE; J. Longo, 

DE; Ph. Novelli, DE; W. Kordulla, DE 

ECC Room 4 

28 

16:50 – 17:10 17:10 – 17:30 17:30 – 17:50 17:50 – 18:10 

UAS 

Chair: A. Schöttl, MBDA/LFK-Lenkflugkörpersysteme, DE 

Certification of Small UAV 

Systems 

C. Battaglia¹; A. Grasso²; R. 

Querzoli¹; G. Orsini²; 

¹Alenia Aeronautica S.p.A., IT; 

²Ministry of Defence, D.G.A.A., IT 

Aircraft Concepts - Future Projects 

Chair: F. Jouaillec, Aerospace Valley, FR 

Estimating Modification 

Efforts for New Aircraft 

Development Projects 

C. Manz, University of Applied 

Siences, DE 

Climatic Aspects 2 

Chair: TBD 

An Efficient Approach to 

GPS/INS Integrity Monitoring 

J. Wendel¹; G. Herbold¹; J. 

Dambeck¹; R. Mönikes²; O. 

Meister²; S. Kiesel²; 

¹MBDA Systems, DE; ²Universität 

Karlsruhe (TH), DE 

Aerodynamic Analysis and 

Design of a Future Air-Speed 

Transit Flying Over the 

Nonplanar Ground Surface 

J. Cho; J. Jeonghyun Cho; 

Hanyang University/School of 

Mechanical Engineering, KR 

Flight Control for Micro Aerial 

Vehicles Using a Modular 

Neural Network Approach 

T. Krüger, Institut für Luft- und 

Raumfahrtsysteme - TU- 

Braunschweig, DE; L. Krüger, 

Mavionics GmbH, DE; A. Kuhn, 

Andata Development 

Technologies, AT; J. Axmann, 

Volkswagen AG, DE; P. 

Vörsmann, Institut für Luft- und 

Raumfahrtsysteme, DE 

The Constant g Stability 

System 

D. F. Reid, NZ 

Room Paris 

Plasma Flyer - The First 

MiniUAV with Plasma Flow 

Control 

B. Göksel, Electrofluidsystems 

Ltd. Holding, DE 

Estrelsaal A 

Configuration Design of a 

Roadable Aircraft fixed a Ring 

Wing 

M. Nakajima; Y. Nishimiya; H. 

Kikukawa; Kanazawa Institute of 

Technology, JP 

ECC Room 4


14:00- 

15:00 


15:10 – 15:50 15:50 – 16:10 16:10 – 16:30 


Details for 




overview 


Details for 




overview 


Chair: N. Gualtieri, Thales Alenia Space, IT 

Development of a Dimensionally Stable CFRP 

Structure for Supporting Optical Instruments 

in a Laser Communication Device 

A. Di Carlo; R. Usinger; Oerlikon Space AG, CH 


Chair: H.J. Baier, TU München, DE 

Polymerisation of Composite Structures in 

Free Space Environment 

G. Nechitailo, Institute of Biochemical Physics, 

Russian Academy of Science, RU; A. Kondyurin, 

University of Sydney, AU 


Chair: TBD 

Estrelsaal C1 

Development of a Dimensionally Stable 

Lightweight Structure for the LISA Pathfinder 

Science Module 

H.P. Gröbelbauer; M. Heer; Oerlikon Space AG, CH 

Estrelsaal C3 

Development and Verification of a High 

Temperature Solar Array Structural Technology 

D. Petry; R. Krautwald; H.G. Schnell; Astrium GmbH, 

DE 

ECC Room 5 

16:50 – 17:10 17:10 – 17:30 17:30 – 17:50 17:50 – 18:10 


Chair: N. Gualtieri, Thales Alenia Space, IT 

A Hierarchical Approach for 

the Buckling Analysis of the 

Vega 1/2 Interstage 

E.L. Jansen¹; J.J. Wijker, Dutch 

Space BV, NL; J. Arbocz¹; 

¹Delft University of Technology, 

NL 

Stochastic Analysis 

Chair: J.N. Bricout, CNES, FR 

Probabilistic Methods Applied 

to Fracture Control of 

Spaceflight Structures. 

G. Sinnema, ESA, NL; C. 

Mattrand, IFMA, FR; F. Marques 

Novo, AOES BV, NL 


Chair: TBD 

The Primary and Secondary 

Structures of ALADIN 

C. Kaiser¹; C. Widani¹; K. Härtel¹; 

P. Haberler¹; O. Lecrenier, EADS 

Astrium SAS, DE; G. Labruyere, 

ESTEC/ESA, DE; 

¹Kayser-Threde GmbH, DE 

PLEIADES HR SATELLITE - 

Mechanical and Thermal 

Architecture 

V. Albouys, CNES, FR; P. 

Corberand, EADS Astrium, FR; 

L. Larue, EADS, FR; S. Andre¹; 

A. Soler¹; 

¹Thales, FR 



29 

Efficient Structural-Thermal- 

Optical Performance Analysis 

Approach 

B. Messerschmidt; B. Specht; 

EADS Astrium, DE 

Identification of Numerical 

Modelling Uncertainty Based 

on Dynamic Fuzzy Finite 

Element Analysis 

D. Moens; M. De Munck; D. 

Vandepitte; K.U.Leuven, BE 

Estrelsaal C1 

Development of a 3D Finite 

Element Model for Distortion 

and Gravitational Analyses of 

a Dimensionally Stable 

Satellite Structure like the 

LISA Pathfinder Science 

Module 

D. Kaiser; T. Pagano; Oerlikon 

Space AG, CH 

Estrelsaal C3 

Stochastic Simulations for the 

Robust Design of Space 

Optical Instruments 

W. Konrad¹; C. Mottl, 

Technische Universität Berlin, 

DE; A. Weber, Technische 

Universität Dresden, DE; S. 

Lucarelli¹; 

¹EADS Astrium GmbH, DE 

ECC Room 5

Thursday, 13th September 2007 

08:30- 

09:30 

Technology Forum (Space) 

09:40 – 10:00 10:00 – 10:20 10:20 – 10:40 10:40 – 11:00 

Air Traffic Management 1 

Chair: A. Geisler, Österreichische Forschungsförderungsgesellschaft, AT 

The Air Traffic Management 

System for 2050: Virtual - 

Global - Automated 

M. B. Brochard, 

EUROCONTROL, FR 

EMMA2 - EUROPEAN 

AIRPORT MOVEMENT 

MANAGEMNT by A-SMGCS, 

Part 2 

M. Roeder, DLR, DE 

Flight Mechanics: Handling Qualities 

Chair: H.-C. Oelker, EADS Military Air Systems, DE 

Aircraft Flying Qualities And 

Flight Safety 

A.V. Efremov; A.V. Koshelenko; 

A.V. Ogloblin; Moscow aviation 

institute, RU 

Optimizing Motion Cueing for 

Research Flight Simulation 

L. Fucke, TU Berlin, DE 

Advanced Maintenance Technologies 1 

Chair: M. Worsfold, Smiths Aerospace, GB 

On-Board Health Assessment 

of an Electro-Mechanical 

Actuator Using Wavelet 

Features 

J. Schaab, TU Darmstadt, DE; U. 

Klingauf, TU-Darmstadt, DE 

Knowledge Space Model 

N. McDonald; R. Morrison; P. 

Grommes; Smiths Aerospace, 

GB 

Augmented Reality 

Technology for Control Tower - 

Analysis of Applicability Based 

on the Field Study 

E. Pinska, EUROCONTROL 

Experimental Centre, FR; C. 

Tijus, FR 

Fine-Tuning Handling Qualities 

on High Performance Fighter 

Aircraft: Maximising Roll 

Acceleration while Avoiding 

Roll-Ratchet 

M. Hanel, EADS Deutschland 

GmbH / EF2000 FJT, Ottobrunn, 

DE; S. Fallon, BAE Systems / 

EF2000 FJT, Ottobrunn, DE 

Hydraulic Actuation Loop 

Degradation Diagnostic and 

Prognostic 

E. Diez-Lledó¹; J. Aguilar-Martin¹; 

J.R. Massé, Hispano-Suiza, FR; 

Griful, Eulàlia, ES; 

¹LAAS-CNRS, FR 

ECC Hall C 

Reliable Traffic Scenarios for 

Very Light Jets and their 

Impact onto the Air Traffic 

Control System 

G. Naumann; T. Guenther; H. 

Fricke; Dresden University of 

Technology, DE 

ECC Hall D 

A Method for Investigation of 

Pilot-Vehicle System 

Dynamics in Wake Vortex 

Encounters 

A. Schönfeld¹; A. V. Efremov, 

Moscow Aviation Institute, RU; 

R. Luckner¹; 

¹ILR, Technical University of 

Berlin, DE 

Estrelsaal B 

Landing Gear Health 

Monitoring 

A. Mortimore, Airbus, GB 

30 

11:20 – 11:40 11:40 – 12:00 12:00 – 12:20 12:20 – 12:40 

Air Traffic Management 2 

Chair: M. Schnell, DLR Oberpfaffenhofen, DE 

ANASTASIA : Airborne New 

and Advanced Satellites 

techniques and Technologies 

in A System Integrated 

Approach 

J.Y. Catros, THALES-Avionics, 

FR 

Advanced Wind Tunnel Testing 

Chair: J. Kooi, DNW, NL 

Noise Source Location in 

Closed Test Sections with 

Acoustic Arrays 

L. Koop, DLR, NL; P. Sijtsma¹; S. 

Oelemans¹; 

¹NLR, NL 

NEWSKY – Networking the Sky 

for Aeronautical 

Communications 

F. Schreckenbach; M. Schnell; S. 

Scalise; German Aerospace 


Benchmarking Pressure 

Sensitive Paint Measurement 

Systems 

D. Hurst, ARA, NL 

Advanced Maintenance Technologies 2 

Chair: M. Worsfold, Smiths Aerospace, GB 

Condition based Operational 

Risk Assessment An 

Innovative Approach To 

Improve Fleet And Aircraft 

Operability, Part 1 

A. Arnaiz, Tekniker, ES; A. 

Schirrmann, EADS Deutschland, 

DE; Z. Papachatzakis, University 

Patras, GR 






A. Schirrmann, EADS 

Deutschland, DE; A. Arnaiz, 

Tekniker, ES; Z. Papachatzakis, 

University Patras, GR 

A Generic Platform for 

Building Air Traffic 

Environmental Internet 

Services 

J.E. Weggemans; J.F.H.W. van 

Weert; National Aerospace 

Laboratory NLR, NL 

Model Deformation 

Measurements in Wind 

Tunnels 

D. Hurst, ARA, NL 






Z. Papachatzaki, University 

Patras, ES; A. Schirrmann, 

EADS Deutschland, DE; A. 

Arnaiz, Tekniker, ES 

ECC Hall C 

NEWSKY - Novel Simulation 

Concepts for Future Air 

Traffic 

C.H. Rokitansky; M. Ehammer; 

T. Gräupl; University of 

Salzburg, AT 

ECC Hall D 

Development of Remote- 

Controls for Movable 

Surfaces of Wind Tunnel 

Models 

J. van Twisk, NLR, NL 

Estrelsaal B 

Cost Benefit Analysis of a 

Health Management System 

H. Fromm; M. Buderath; EADS 

Deutschland GmbH / EF2000 

FJT, Ottobrunn, DE


08:30- 

09:30 


09:40 – 10:00 10:00 – 10:20 10:20 – 10:40 10:40 – 11:00 

Aircraft Composite Structures 

Chair: S. Pantelakis, University of Patras, GR 

ALCAS - Advanced Low Cost 


D. Phipps, Airbus, GB 

Space Systems: Technology Aspects 

Chair: TBD 

Reinhard-Furrer-Preis für 

eine herausragende 

Dissertation zum Thema: 

Die Modellierung der Natrium- 

Kaliumtropfen als Beitrag zu 

orbitalen Objektpopulation 

C. Wiedemann, TU 

Braunschweig, DE 

ALCAS Centre Wing Box - Low 

Cost LCM Stringer 

Manufacturing 

M. Kleineberg, DLR, DE; M. 

Schradick, Airbus, DE; E. 

Sperlich, ZIM, DE 

The Advanced ISS Air Monitor 

ANITA - In Orbit Operations 

T. Stuffler¹; G. Tan, ESA, NL; A. 

Honne²; H. Mosebach¹; D. 

Kampf¹; H. Odegard²; N. Henn, 

DLR, DE; 

¹Kayser-Threde GmbH, DE; 

²SINTEF, NO 

Aero-Engine Control and Measurement Techniques 

Chair: S. Staudacher, Universität Stuttgart, DE 

Application of Fuzzy-Logic 

Controller in Gas Turbine 

Speed Control and Surge 

Control on Transient 

Performance 

A.A. Torghabeh; A.M. Tousi; 

Amirkabir University, IR 

Dynamische Modellbildung 

und Reglerentwurf für ein 

Hybridsystem bestehend aus 

Mikrogasturbine und SOFC- 

Brennstoffzelle 

F. Kroll; A.E. Nielsen; S. 

Staudacher; Institut für 

Luftfahrtantriebe, Universität 

Stuttgart, DE 

Crashworthiness of Composite 


G. Labeas, University of Patras, 

GR 

Spacecraft Disturbances 

Induced by Hypervelocity 

Impacts - Application to GAIA 

Spacecraft 

J.B. Vergniaud¹; M. Guyot¹; M. 

Lambert, ESA, NL; F. Schafer²; 

S. Ryan²; S. Hiermaier²; E. 

Taylor, Open University, GB; 

¹EADS Astrium, FR; ²EMI, DE 

Installation Effects 

Characterisation of a Typical 

High Bypass Ratio Engine 

Using Numerical Simulations 

and Particle Image Velocimetry 

A. Vuillemin, Snecma, FR; O. 

Piccin, ONERA GMT, FR; R. 

Davy, ONERA DSNA, FR; F. 

Crosta, Airbus France, FR 

ECC Room 2 

New Challenges in Structural 

Design and Analysis of 

Composite Structures 

C. Petiot, EADS France, FR 

ECC Room 3 

Orbit Error Estimations for 

ESA’s Collision Risk 

Prediction Service 

H. Krag¹; H. Klinkrad¹; J.-R. 

Alarcón-Rodríguez, GMV S. A., 

ES; 

¹ESA/ESOC, DE 

ECC Room 1 

Winfried Bierhals-Stiftungspreis 

für die Diplomarbeit zum Thema: 

Anwendung der 

Schallemissionsprüfung an 

thermisch hochbelasteten 

Brennkammerschindeln 

F. Meinl, University Karlsruhe, 

DE 

31 

11:20 – 11:40 11:40 – 12:00 12:00 – 12:20 12:20 – 12:40 

Aircraft Composite Structures / Structures - Analysis 1 

Chair: TBD 

Experimental and 

Computational Studies of 

Mechanically Fastened Joints 

in Composite Aircraft 

Structures 

M. McCarthy, University of 

Limerick, IE 

Reentry and Landing 

Chair: TBD 

Landing Pallet: a Crushable 

Mission to Mars 

P. Palmieri, Thales Alenia Space, 

IT 

Finite Element Unit Cell Based 

Strength Prediction of Stitched 

CFRP Laminates 

H. Heß; N. Himmel; Institut für 

Verbundwerkstoffe GmbH (IVW), 

DE 

The Hypersonic Drag Balloon 

ARCHIMEDES and its 

Research and Testing Program 

H.S. Griebel¹; B. Häusler¹; C. 

Mundt, Institute of 

Thermodynamics, UniBw 

München, DE; H. Rapp, Institute 

of Light Weight Structures, 

UniBw München, DE; H.J. 

Gudladt, Institute of Material 

Sciences, UniBw München, DE; 

¹Institute of Space Technology, 

UniBw München, LRT9, DE 

Hypersonic Propulsion Systems 

Chair: J. von Wolfersdorf, Universität Stuttgart, DE 

Recent Progress in 

Scramjet/Rocket based 

Combined Cycle Engines at 

JAXA, Kakuda Space 

Propulsion Center 

S. Ueda; S. Sato; K. Itoh; K. Tani; 

S. Tomioka; T. Kanda; JAXA, JP 

Non-Deterministic Analysis of 

a Scramjet Propulsion System 

G. Schütte; S. Staudacher; 

Institute of Aircraft Propulsion 

Systems/University of Stuttgart, 

DE 

MT Aerospace Innovationspreis 

für die Diplomarbeit zum Thema: 

Bruchmechanische 

Untersuchung neuartiger, 

nichtrechtwinkliger 

Strukturversteifungskonzepte 

im Vergleich zur 

konventionellen rechtwinkligen 

Flugzeugrumpfversteifung 

S. Kébreau, TU Braunschweig, 

DE 

Landing Impact Simulation and 

Testing Approaches-alcatel 

Alenia Space Experience 

P.C. Marucchi-Chierro, Alcatel 

Alenia Space-Italy, IT; R. Riva, 

SOFITER SYSTEM 

ENGINEERING, IT; R. Ullio, 

Alcatel Alenia Space-Italy, IT; F. 

Quagliotti, Alcatel Alenia Space - 

Italy, IT 

Experimental Study of the 

Single Expansion Ramp Nozzle 

Flow Properties and its 

Interaction with the External 

Flow 

C. Hirschen; A. Gülhan; German 


ECC Room 2 

Innovative Approaches for 

Integration of Functions in 

Composite Sandwich 

Structures by the Example of 

Cabin Interior 

M. Pein; D. Krause; T. 

Gumpinger; TU Hamburg- 

Harburg, DE 

ECC Room 3 

Re-entry Risk Assessment for 

Launchers - Development of 

the New SCARAB 3.1L 

T. Lips¹; B. Fritsche¹; M. 

Homeister¹; G. Koppenwallner¹; 

H. Klinkrad, ESA/ESOC, DE; M. 

Toussaint, ESA/HQ, FR; 

¹HTG, DE 

ECC Room 1 

Optimizing Aircraft 

Maintenance Efficiency in 

Global Start-up Support 

Projects 

S. Hollmeier, C. Winck, 

F. Mayer, Lufthansa Technik, 

Frankfurt, DE


08:30- 

09:30 


09:40 – 10:00 10:00 – 10:20 10:20 – 10:40 10:40 – 11:00 

UAS - Sensors and Signal Processing 

Chair: G. Trommer, Universität Karlsruhe, DE 

Optimal Manoeuvre Change- 

Detection of Agile Aerial 

Systems 

A. Schöttl, MBDA/LFK- 

Lenkflugkörpersysteme, DE 

Aerodynamics 2 

Chair: TBD 

Numerical Simulation of the 

Flow around Circulation 

Control Airfoils 

K.-C. Pfingsten; C. Jensch; R. 

Radespiel; TU Braunschweig, DE 

Micro – Nano Technologies 1 

Coordinator: E. Kircher, ESA/ESTEC, NL 

Implementation of a Sense and 

Avoid System for Unmanned 

Aerial Vehicles 

J.-B. Park; P. Vörsmann; Institute 

of Aerospace Systems, TU 

Braunschweig, DE 

Airbus-Preis der EADS Airbus 

GmbH für die Dissertation zum 

Thema: 

Experimentielle Untersuchungen 

zur Effizienz der aktiven 

Strömungskontrolle an einer 

Hochauftriebskonfiguration 

R. Petz, TU Berlin, DE 

Sensor Suites for Future 

Autonomous Unmanned Aerial 

Vehicles 

T. Rapp; D. Hoffmann; EADS, 

DE 

Analysis of Plume Impact on 

Launch Tower During Lift Off 

R. Sala¹; M. Galeotta¹; A. 

Veneziani²; L. T. De Luca²; 

¹Carlo Gavazzi Space, IT; 

²Politecnico Milano, IT 

Room Paris 

Stereo-Based Obstacle 

Mapping from a Helicopter 

Platform 

F. Andert; L. Goormann; 

Deutsches Zentrum für Luft- und 

Raumfahrt, DE 

Estrelsaal A 

DLR-Technologiepreis für 

Arbeiten auf dem Gebiet der 

Segelflugtechnik für die 


Bestimmung des laminarturbulenten 

Grenzschichtumschlags auf 

Tragflügeln im Windkanal und 

im Freiflug mittels 

Thermografie 

A. Wagner, TU Dresden, DE 

ECC Room 4 

32 

11:20 – 11:40 11:40 – 12:00 12:00 – 12:20 12:20 – 12:40 

Flight Control - Actuation 

Chair: D. Scholz, HAW Hamburg, DE 

Servounterstützte Steuerung 

von Segelflugzeugen (Servo- 

Boosted Control Elements for 

Sailplanes) 

A. Gäb; J. Nowack; W. Alles; 

RWTH Aachen University, DE 

Cabin architecture 

Chair: L. Jonson, SAS, SE 

Airbus Innovative Cabin 

Design 

K.D. Kricke; I. Wuggetzer; Airbus 


Micro – Nano Technologies 2 

Coordinator: E. Kircher, ESA/ESTEC, NL 

Adaptive Internal Model 

Control Using Laguerre Series 

Representation for a Decentral 

Flap Actuation System 

O. Meckel, Flugsysteme und 

Regelungstechnik, TU 

Darmstadt, DE 

Electrical Passenger Door 

Concepts 

W. Buchs; J. Margraf; Eurocopter 


Position and Load Control for 

Hybrid Primary Flight Controls 

with Electromechanical and 

Electrohydraulic Actuators 

O. Cochoy; U. B. Carl; 

F. Thielecke; Hamburg 

University of Technology, DE 

PAXMOV-Passenger 

Movement Behaviour Model for 

Future Passenger-orientated 

Long-haul Aircraft Cabin 

Design 

K.O. Ploetner, Institute of 

Aeronautical Engineering - TU 

München, DE 

Room Paris 

The Power Electronic 

Environment on More Electric 

Aircrafts A Way to Improve 

Signal Integrity by means of 

Shielded Cables 

R. Tiedemann; D. Giugno; Rolls- 

Royce Deutschland, DE 

Estrelsaal A 

RODON®’s Diagnostic 

Methods for New Generic 

System BITE Architectures 

B. Kadmiry, Soerman 

Information & Media AB, SE; 

D. Geiter, Airbus Deutschland, 

avionic dept., DE 

ECC Room 4


08:30- 

09:30 


09:40 – 10:00 10:00 – 10:20 10:20 – 10:40 10:40 – 11:00 


Chair: P. Mourey, CNES, FR 

AlphaBus, the European High 

Capacity Platform for SatComs 

S. Massier¹; G. Lubrano¹; P. 

Belliol, EADS Astrium, FR; A. 

Obst, ESA/ESTEC, NL; L. 

Petitjean, CNES, FR; 

¹Thales Alenia Space, FR 

Materials and Active Structures 1 

Chair: H.J. Baier, TU München, DE 

High-Temperature Oxidation of 

SSiC in Plasma Flows 

T. Laux, German Aerospace 

Center, DE 


Chair: TBD 

Stiftungspreis der IABG für die 


Untersuchung und Anwendung 

der Monte Carlo Simulation zur 

Auslegung robuster 

Raumfahrtstrukturen 

A. Weber, TU Dresden, DE 

Active Flatness Control Of 

Membrane Structures With 

Consideration Of Nonlinear 

Dynamics 

Y.-R. Hu; X. Wang; W. Zheng; 

Canadian Space Agency, CA 

Thermal Management Issues 

for Multifunctional Solar 

Arrays 

J.A. Foster; G.S. Aglietti; 

University of Southampton, 

School of Engineering Sciences, 

GB 

Strength Aspects for the 

Design of ZERODUR Glass 

Ceramics Structures 

S. Lucarelli¹; P. Gath¹; P. 

Hartmann²; K. Nattermann²; T. 

Doehring²; 

¹EADS Astrium GmbH, DE; 

²Schott AG, DE 

Estrelsaal C1 

Innovation in Structures 

Engineering for Future 

Launch Vehicles - Facing the 

21st Century Challenges 

J. Martin, EADS CASA Espacio, 

ES 

Estrelsaal C3 

On the Design of Active 

Mirrors with PZT Bimorph 

Actuation 

A. Preumont¹; G. Rodrigues¹; R. 

Bastaits¹; Y. Stockman, Centre 

Spatial de Liège, BE; P. Villon, 

Université de Technologie de 

Compiègne, FR; 

¹Active Structures Laboratory - 

Université Libre de Bruxelles, 

BE 

ECC Room 5 

11:20 – 11:40 11:40 – 12:00 12:00 – 12:20 12:20 – 12:40 

Structural Dynamics & Microvibrations 1 

Chair: M. Sinapius, DLR Braunschweig, DE 

Micro-Vibration Measurements 

on Thermally Loaded Multi- 

Layer Insulation Samples 

A. Grillenbeck, IABG, DE; B. 

Pouilloux, CNES, FR 

Mechanical Testing 1 

Chair: J.B. Bernaudin, EADS Astrium, FR 

Mechancial Qualification of the 

Herschel Satellite 

M. v. Alberti, EADS Astrium, DE; 

Y. Roche, Alcatel Alenia Space, 

FR; W. Teichert, European 

Testing Services, NL; A. 

Schnorhk, European Space 

Agency, NL 


Chair: TBD 

A Process with Quantified 

Accuracy for Predicting 

Electronic Equipment Vibration 

Response 

R. A. Amy¹; G. S. Aglietti¹; G. 

Richardson, Surrey Satellite 

Technology Limited, GB; 

¹School of engineering sciences, 

University of Southampton, GB 

Optical Methods for Non 

Contact Measurements of 

Membranes Space Structures 

S. Roose¹; Y. Stockman¹; T. 

Kuhn²; H. Baier²; S. Langlois, 

ESTEC, European Space 

Agency, NL; G. Casarosa, AOES 

Group BV, NL; 

¹Centre Spatial de Liège, BE; 

²Lehrstuhl für Leichtbau, 

Technische Universität München, 

DE 



33 

Aeroelastic Prediction and 

Validation Methods for USV1 

M. Belardo; L. Di Palma; M. 

Pecora; CIRA Scpa, IT 

Recent Achievements for the 

Mechanical Data Handling at 

IABG 

A. Grillenbeck; S. Dillinger; S. 

Prause; IABG, DE 

Estrelsaal C1 

Local Damping Identification 

from Spacecraft Sine Test 

G. Ladurre¹; A. Carpine¹; R. 

Redondo, CNES, FR; 

¹Thales Alenia Space, FR 

Estrelsaal C3 

SmosPlm Mechanical 

Qualification Tests 

M.A. Gil; J.M. Bajo; M.A. Plaza; 

EADS CASA Espacio, ES 

ECC Room 5


14:00- 

15:00 

Aeronautical Orientation and Technology Needs 

15:10 – 15:30 15:30 – 15:50 15:50 – 16:10 16:10 – 16:30 

Air Transport Research and Technology 

Chair: J. Reichmuth, DLR Köln, DE 

Thinking Out of the Box 

A. de Graaff, AD Cuenta, NL 

Multiobjective Particle Swarm 

Optimization Technique as an 

Effective Tool for Aircraft 

Requirements Analysis 

L. Blasi; S. Barbato; L. Iuspa; 

Second University of Naples - 

DIAM, IT 

Technologies for Highspeed Transport 1 

Chair: M. Mallet, Dassault Aviation, FR 

Noise Prediction for SSBJs 

R.H. Self, University of 

Southampton, GB 

Development of MDO 

Techniques for the Design of a 

SSBJ 

M. Ravachol, Dassault Aviation, 

FR; K. Giannakoglou, NTUA, GR 

Fault Detection in A/C Systems 

Chair: F. Thielecke, DLR Braunschweig, DE 

Performance Degradation 

Analysis of Fault Tolerant 

Aircraft Systems 

C. Raksch; R. van Maanen; D. 

Rehage; F. Thielecke; Hamburg 

University of Technology, DE 

Fault Detection and Isolation of 

Actuator Failures for a Large 

Transport Aircraft 

A. Varga, DLR, DE 

CELINA - Fuel Cell Application 

In A New Configured Aircraft 

C. Schilo, Airbus Deutschland, 

DE 

The Challenges of an 

"Acceptable" Sonic Boom 

F. Coulouvrat, CNRS, FR 

Model-Based Failure Detection 

of a Trimmable Horizontal 

Stabilizer Actuator with Two 

Primary Load Paths 

N. Wachendorf; U.B. Carl; F. 

Thielecke; TUHH/FST, DE 

ECC Hall C 

Trajectory Optimization of a 

Solar Aircraft for Performance 

Improvement 

G. Sachs¹; J. Lenz¹; H. Ross, 

IBR, DE; 

¹Institute of Flight Mechanics 

and Flight Control of TU 

München, DE 

ECC Hall D 

Alternative Engine 

Technologies for Supersonic 

Propulsion 

A. Vuillemin; P. Coat; Snecma, 

FR 

Estrelsaal B 

Predictive Maintenance in 

Avionics 

S. Ghelam; M. Feuillebois; M. 

Glade; J.P. Derain; 

EUROCOPTER, FR 

34 

16:50 – 17:10 17:10 – 17:30 17:30 – 17:50 17:50 – 18:10 

Industrial and Research Cooperations 

Chair: S. Eelman, TU München, DE 

EREA, the association of 

European Research 

Establishments in Aeronautics 

F.J. Abbink, EREA, NL 

GARTEUR: Long Term R&T 

collaboration in Europe 

L. Vecchione; V. Puoti; CIRA, 

Italian Centre for Aerospace 

Research, IT 

Technologies for Highspeed Transport 2 

Chair: M. Mallet, Dassault Aviation, FR 

Climate Impact of a Potential 

Supersonic Fleet 

V. Grewe, DLR 

Oberpfaffenhofen, DE 

Supersonic Laminar Flow 

Control Investigations within 

the SUPERTRAC Project 

D. Arnal, ONERA, FR 

Measurement Methods for Aerodynamics 

Chair: TBD 

The TELFONA Pathfinder Wing 

for the Calibration of the ETW 

Wind Tunnel 

G. Schrauf, Airbus, DE; K.H. 

Horstmann¹; T. Streit¹; 

¹DLR, DE 

Stereo-PIV and Hot-Wire 

Investigations on Delta Wing 

A. Furman; C. Breitsamter; 

Technische Universität München, 

DE 

Aerospace Valley: The Cluster 

Effect Applied to the 

Aerospaec Industry in South 

Western France 

F. Jouaillec, Aerospace Valley, 

FR 

Automatic Shape Design for 

Low Boom and Low Drag High 

Speed Transport 

V. Selmin, Alenia Aeronautica, IT 

Aerodynamic Optimization and 

Boundary Layer Control 

L. Popelka, Academy of Sciences 

of the Czech Republic, CZ; M. 

Matejka, Czech Technical 

University in Prague, CZ 

ECC Hall C 

Development of Principles 

and Rules for Sustaining 

Aircraft Airworthiness in 

Developing Countries 

MFA. Odutola; C.O. Edeh; 

Nigerian College of Aviation 

Technology, NG 

ECC Hall D 

Solution of the Euler 

Equations for the Prediction 

of the Sonic Boom 

A. Dervieux, INRIA, FR 

Estrelsaal B 

Wolfgang Heilmann-Preis der 

MTU GmbH für die 


Background Oriented 

Schlieren - Möglichkeiten und 

Grenzen des optischen 

Verfahrens zur quantitativen 

Dichtegradientenbestimmung 

T. Nafz, University Karlsruhe, 

DE


14:00- 

15:00 


15:10 – 15:30 15:30 – 15:50 15:50 – 16:10 16:10 – 16:30 

Structures: Buckling 

Chair: TBD 

Buckling analysis and 

Qualification static load testing 

of VEGA Interstage 1/2 

structure 

J.F. Tyrrell; J.W. Cremers; Dutch 

Space B.V., NL 

Galileo 

Chair: TBD 

Galileo Evolution: Enhanced 

Error Correction Strategies 

and Integrity Assessments 

B. Belabbas¹; S. Graf, TU 

München, DE; P. Rémi¹; M. 

Meurer¹; 

¹DLR, DE 

Probabilistic Approach for 

Improved Buckling Knock- 

Down Factors of CFRP 

Cylindrical Shells 

R.D. Degenhardt¹; A. Bethge¹; A. 

Kling¹; R. Zimmermann¹; K. 

Rohwer¹; J. Tessmer¹; A. Calvi, 

ESA/ESTEC, NL; 

¹DLR, DE 

The GIOVE-A Mission - A Major 

Step Towards Galileo 

B. Kleine Schlarmann; M. 

Falcone; J. Hahn; M. Hollreiser; 

ESA/ESTEC, NL 

Aero Engine Components Exhaust System / Propeller 

Chair: R. Lederer, MTU Aero Engines, DE 

Numerical Simulation of Mixed 

Jet Exhaust System and its 

Verification 

J.A. Lieser; B. Deinert; C. Möller; 

F. Müller; Rolls-Royce 


Experimental and Numerical 

Investigations of the Mixing 

Flow in Turbofan Engines in 

the Sub-Idle Operating Range 

B. Banzhaf; S. Staudacher; 

Institut für Luftfahrtantriebe, 


Buckling of Multilayered Metal 

Composite Domes 

J. Blachut; P. Smith; The 

University of Liverpool, GB 

BayNavTech - Monitoring 

GNSS Performance for 

Demanding Applications 

C. Schäfer; J. Vilzmann; M. 

Söllner; R. Kohl; EADS Astrium, 

DE 

Thrust Reverser Aerodynamic 

Design: CFD Analysis and 

Comparison with Experiments 

D. Kliche¹; R. Spieweg²; R. 

Schweikhard²; C. Mundt¹; 

¹Universität der Bundeswehr 

München, DE; ²Rolls-Royce 

Deutschland Ltd & Co KG, DE 

ECC Room 2 

Efficient Buckling Analysis of 

Stiffened Composite Airframe 

Parts 

C. Mittelstedt, AIRBUS 


ECC Room 3 

First Outdoor Positioning 

Results with Real Galileo 

Signals by Using the German 

Galileo Test and Development 

Environment - GATE 

G. Heinrichs¹; E. Löhnert¹; E. 

Wittmann¹; R. Kaniuth, 

University FAF Munich, DE; 

¹IFEN GmbH, DE 

ECC Room 1 

Aerodynamic Analysis and 

Design of a Propeller for MAV 

Propulsion 

J. Cho, Hanyang 

University/School of Mechanical 

Enginnering, KR; S. Lee¹; L. 

Cho¹; 

¹Hanyang University/Department 

of Mechanical Enginnering, KR 

35 

16:50 – 17:10 17:10 – 17:30 17:30 – 17:50 17:50 – 18:10 

Structures: Analysis 2 

Chair: TBD 

FEA Approach for the 

Prediction of the Void’s Effects 

on the Elastic Properties of 

Unidirectional Fiber Reinforced 

Composites 

L. Mormile¹; F. Romano²; A. 

Riccio²; L. Iuspa¹; 

¹Second University of Naples, IT; 

²CIRA, IT 

Postbuckling Modeshapes of 

Composite Stiffened Fuselage 

Panels Incorporating 

Stochastic Variables 

M.C.W. Lee, University of New 

South Wales, AU; D.W. Kelly, 

University of New South Wales 

School of Mechanical and 

Manufacturing Engineering, AU; 

A.C. Orifici, School of Aerospace, 

Mechanical & Manufacturing 

Engineering, RMIT University, 

AU; R.S. Thomson, Cooperative 

Research Centre for Advanced 

Composite Structures Limited, 

AU 

Supersonic/Hypersonic Flow: Reentry 

Chair: W. Kordulla, European Space Agency, ESA/ESTEC, NL 

In flight Aerodynamic 

Experiment for the Unmanned 

Space Vehicle FTB-1. 

G. C. Rufolo; M. Marco; R. 

Pietro; B. Salvatore; CIRA, IT 

Aero(thermo)dynamic CFD 

Analyses of Various Re-Entry 

Capsule Shapes in 

Comparison to Recent Test 

Results 

H.P. Noeding, EADS Astrium, 

DE; R.C. Molina, ESA-ESTEC, 

NL 

Aero-Engine Economic Design, Manufacturing and Maintenace 

Chair: S. Staudacher, Universität Stuttgart, DE 

Empowering Engine 

Engineers: Advancing the 

State-of-the-Art in 

Collaborative Multi-National 

Multidisciplinary Engine 

Design 

E. Kesseler¹; P. Arendsen¹; M.H. 

van Houten¹; R. Parchem²; B. 

Meissner²; M. Nagel³; J. Barner³; 

H. Wenzel, Engineous, DE; 

¹NLR, NL; ²Rolls Royce, DE; 

³MTU Aero Engines, DE 

Production Cost Estimation of 

the aeroengines in VITAL 

O.M.F. Arago; S. Bretschneider; 

S. Staudacher; Stuttgart 

University, DE 

FEM Simulation of the Inflicted 

Delamination to IMC Laminated 

Composites during 

Manufacturing Process 

S. Khosoussi; M. Rezaei; A. 

Abedian; Sharif University of 

Technology, IR 

Advanced Aerothermodynamic 

Analysis of SHEFEX 

T. Barth, DLR, DE 

Market-oriented Blisk 

Manufacturing 

A Challenge for Production 

Engineering 

E. Bayer; M. Bußmann; MTU 

Aero Engines GmbH, DE 

ECC Room 2 

Finite Element Analysis of 

Superplastic Behavior of 

MMCs in Presence of Some 

Manufacturing Defects 

A. Barakati; A. Abedian; M.A. 

Kouchakzadeh; Sharif University 

of Technology, IR 

ECC Room 3 

The Pre-x Lifting Body 

Computational Fluid 

Dynamics and Wind Tunnel 

Test Campaign 

P. Baiocco¹; S. Guedron¹; J. 

Oswald¹; D. Ponziani¹; F. 

Delattre²; E. Cosson²; J.P. 

Tribot³; A. Bugeau³; 

¹CNES, FR; ²ASTRIUM, FR; 

³Dassault Aviation, FR 

ECC Room 1 

Global Trends in the Industry 

of Commercial Aircraft Engine 

Maintenance 

P. Schumacher, MTU 

Maintenance Berlin- 

Brandenburg GmbH, DE


14:00- 

15:00 


15:10 – 15:30 15:30 – 15:50 15:50 – 16:10 16:10 – 16:30 

UAS - Unmanned Helicopters 

Chair: F. Thielecke, DLR Braunschweig, DE 

ARTIS - An Interdisciplinary 

Unmanned Rotorcraft Flight 

Test Demonstrator 

J.S. Dittrich, DLR Institute of 

Flight Systems, DE 

UAV VTOL-Research Testbed - 

SHARC’ 

O. Heinzinger; R. Arning; EADS 

Germany Innovation Works, DE 

Cabin Enviromental Control System Simulation and Test 

Chair: G. Konieczny, Airbus Deutschland, DE 

Stability of the Air Flow in a 

Two Aisle Cabin Model 

C. Wagner; M. Kühn; J. Bosbach; 


New Technologie for Earth Observation 

Chair: K. Brieß, TU Berlin, DE 

The Rubin Testbed for In-Orbit 

Verification of Micro- and 

Nanotechnologies 

B. Ziegler, B. Penné, OHB 

Systems, Bremen, DE; I. Kalnin, 

University Bremen, DE 

Dynamic Simulation of 

Innovative Aircraft Air 

Conditioning 

D. Scholz¹; C. Müller¹; T. Giese, 

Airbus Deutschland GmbH, DE; 

M. Haaren, CeBeNetwork GmbH, 

DE; 

¹HAW Hamburg, DE 

Very High Resolution SAR & 

Optical Missions for Future 

Earth Observation 

Applications 

B. Penné, C. Tobehn, M. 

Kassebom, S. Mahal, R. 

Greinacher, OHB Systems, 

Bremen, DE 

VTOL-MAV for Security and 

Rescue Operations with 

Enhanced Geo-Positioning 

Capabilities 

R. Mönikes; N. Frietsch; O. 

Meister; G.F. Trommer; 

University of Karlsruhe, DE 

A Flexible Toolkit for the 

Design of Environmental 

Control System Architectures 

M. Sielemann, DLR, Institute of 

Robotics and Mechatronics, DE 

The Rubin Testbed for In-Orbit 

Verification of Micro- and 

Nanotechnologies 

B. Ziegler, B. Penné, OHB 

Systems, Bremen, DE; I. Kalnin, 

University Bremen, DE 

Room Paris 

A Sequence and Supervisory 

Control System for Onboard 

Mission Management of an 

Unmanned Helicopter 

F.M. Adolf, German Aerospace 

Center (DLR), Institute of Flight 

Systems, DE; F. Thielecke, 

Hamburg University of 

Technology, Institute of Aircraft 

Systems Engineering, DE 

Estrelsaal A 

The New Pressurised 

Fraunhofer Flight Test Facility 

Offered to the Scientific Cabin 

Environment Network 

E. Mayer; G. Grün; R. Hellwig; 

A. Holm; Fraunhofer-Institut für 

Bauphysik, DE 

ECC Room 4 

Very High Resolution SAR & 

Optical Missions for Future 

Earth Observation 

Applications 

B. Penné, C. Tobehn, M. 

Kassebom, S. Mahal, R. 

Greinacher, OHB Systems, 

Bremen, DE 

36 

16:50 – 17:10 17:10 – 17:30 17:30 – 17:50 17:50 – 18:10 

UAS - Autonomous Flight 

Chair: U. Klingauf, TU Darmstadt, DE 

GARTEUR FM AG14 - 

Autonomy in UAVs - A 

Collaborative Research Forum 

Overview 

J.T. Platts, QinetiQ, GB 

Development of an 

Autonomous Avoidance 

Algorithm for UAVs in General 

Airspace 

J. van Tooren, EADS MAS, DE; 

M. Heni, ATENA, DE; J. Beck¹; 

A. Knoll¹; 

¹EADS, DE 

Cabin - Acoustics 

Chair: K.-D. Kricke, Airbus Deutschland, DE 

High Soundproofing Ability of 

Porous Materials under Stress 

Using 4S Technology 

K.E. Thorbeck, TU-Berlin, DE; D. 

Rakov, Russian Academy of 

Science / IMASH, RU 

TBD 

Chair: TBD 

Mock-up of a Loadmaster Area 

for Acoustic Ground Tests 

S. Böhme¹; D. Sachau¹; T. 

Kletschkowski¹; H. Breitbach, 

Airbus Germany GmbH, DE; 

¹Helmut-Schmidt-University, DE 

UAV/UCAV Navigation 

Systems - Present and 

Potential Future 

R.K. Arning; A. Langmeier; E. 

Stenzel; EADS Germany 

Innovation Works, DE 

Influence of noise and 

vibration on the perception of 

the ambience inside the cabin 

V. Mellert, University Oldenburg, 

DE 

Room Paris 

Fast Image Based Landing 

Field Detection 

R.M. Leitner; O. Heinzinger; 

EADS Germany Innovation 

Works, DE 

Estrelsaal A 

Audio Interior for Light 

Aircraft 

O. Pabst; F.T. Tsafak; T. 

Kletschkowski; D. Sachau; 

Helmut-Schmidt- 

University/University of the 

Federal Armed Forces, DE 

ECC Room 4


14:00- 

15:00 


15:10 – 15:30 15:30 – 15:50 15:50 – 16:10 16:10 – 16:30 

Structural Dynamics & Microvibrations 2 

Chair: A. Grillenbeck, IABG, DE 

The Integration of Modal 

Analysis in Vibration 

Qualification Testing 

L. Britte¹; B. Peeters¹; J. M. 

Komrower, LMS North America, 

US; M. O’Grady²; R. Singhal²; 

¹LMS International nv., BE; 

²Canadian Space Agency, CA 

Mechanical Testing 2 

Chair: P. Mourey, CNES, FR 

New Large Mass Property 

Measurement Facility: 

Experience with First Three 

Test Specimens 

W.H. Teichert; G. Slagter; ETS, 

NL 


Chair: TBD 

Feasibility Study of 

Acceleration Limit Substitution 

of Force Limit Vibration Test 

K. Nagahama, Japan Aerospace 

Exploration Agency, JP; S. Shi¹; 

T. Iwasa¹; M. Saitoh¹; 

¹JAXA, JP 

Mechanical Testing on Large 

Aircraft Structures: 

Possibilities - Limits - 

Examples 

R. Baumgartl, IABG, DE 

Non-Linear Dynamics on Space 

Structures at Low Frequencies 

O. Eygonnet, EADS Astrium 

Satellites, FR; R. Redondo, 

CNES, FR 

Qualification Tests of Eurostar 

3000 XL Central Tube 

P. Luengo; P. Brotons; EADS 

CASA Espacio, ES 

Estrelsaal C1 

Development of Failsafe and 

Vibration Damping Flexural 

Feet for Sensitive Space 

Instrument 

E. Bigot; A. Di Carlo; Oerlikon 

Space AG, CH 

Estrelsaal C3 

Application of Component 

Notching and Force Limiting 

Techniques in FORMOSAT-3 

Satellite 

J.C. Kuo; M.C. Cheng; C.W. 

Chou; L.C. Yen; National Space 

Organization, TW 

ECC Room 5 

16:50 – 17:10 17:10 – 17:30 17:30 – 17:50 17:50 – 18:10 

Materials and Active Structures 2 

Chair: M. Klein, European Space Agency, ESA/ESTEC, NL 

Development of Electro Active 

Polymers Configurations to 

Monitor and Control 

Deployable Space Structures 

S. Baldacci¹; F. Thurecht²; E. K. 

Pfeiffer²; P. Sommer Larsen, 

RISOE National Lab., DK; F. 

Carpi³; D. De Rossi³; L. Lampani*; 

P. Gaudenzi*; L. Serafini¹; V. S. 

Zolesi¹; 

¹Kayser Italia srl, IT; ²HIGH 

PERFORMANCE SPACE 

STRUCTURE SYSTEMS GMBH, 

DE; ³Centro Piaggio - Pisa 

University, IT; *DIAA - University 

of Rome La Sapienza, IT 

Production of Gamma Tial 

Based Alloys by Combustion 

Synthesis+Compaction Route 

for Space Rocket Engine 

Complex Parts 

J. Coleto¹; I. Agote¹; M. García de 

Cortazar¹; M. Lagos¹; L. 

Pambaguian, ESA-ESTEC, NL; 

A. Sargsyan¹; V.L. Kvanin²; N.T. 

Balikhina²; I.P. Borovinskaya²; 

S.G. Vadchenko²; A.E. Sytschev²; 

¹TECNALIA-AEROSPACE, ES; 

²Institute of Structural 

Macrokinetics and Materials 

Science Russian Academy of 

Sciences, RU 


Chair: H. Bansemir, Eurocopter Deutschland, DE 

Alphabus Central Tube - 

Development and 

Manufacturing of the Bread 

Board Model 

J. Trigo, EADS CASA ESPACIO, 

ES 


Chair: TBD 

Faserverbundwerkstoffe für 

Weltraumapplikationen 

hergestellt in DP-RTM 

H. Assing; M. Kleineberg; C. 

Sickinger; L. Herbeck; DLR, DE 



37 

Phase Change Materials and 

Thermosensitive Painting: 

Application on Smart Thermal 

Protection Systems 

J. Coleto¹; J. Maudes¹; T. 

Salmon, EADS-ST, FR; L. 

Martinez, LISAP, FR; A. Passaro, 

ALTA SpA., IT; H. Ritter, ESA- 

ESTEC, NL; 

¹TECNALIA-AEROSPACE, ES 

Radiation Attenuation of CFRP 

Wolfram Laminate Structures 

T.J. Brander, Helsinki University 

of Technology/Laboratory of 

Lightweight Struktures, FI; F. 

Garcia, Helsinki Institute of 

Physics (HIP), FI 

Estrelsaal C1 

Time Influence on Viscoelastic 

Materials: Experience 

Feedback on Applications in 

the Space Field 

M. Lathuiliere¹; D. Martin de 

Argenta¹; D. Givois¹; R. 

Redondo, CNES, FR; 

¹01dB-METRAVIB, FR 

Estrelsaal C3 

Passive Damping of 

Spacecraft Sandwich Panels 

M. Romberg, OHB-System AG, 

DE; C. Pereira, RUAG 

Aerospace, CH; M. Kröger, IDS 

Hannover, DE 

ECC Room 5


Chair: TBD 

CEAS-2007- 

Identification System of Aircraft Gas Turbine Engine's Temperature Condition 

A. Sadiqov; M.P. Arif; D.A. Djahangir; S.A. Parviz; National Academy of Aviation, AZ 


Experimental Investigation of Frontal Device for Perspective Combustors 

V.B. Rutovskiy; I.V. Kravchenko; D.P. Tkachenko; M.N. Boulaeva; Moscow Aviation Institute (State Technical University), 

RU 


Terrain Following Minimum Time Trajectory Design for UAV Swarms Using Mixed Integer Programming 

J.W. Vervoorst; T. Kopfstedt; Diehl BGT Defence GmbH & Co. KG, DE 


Cabin Electrical Installation for BWB Aircraft 

O. Zysk, QualityPark AviationCenter, DE 


Garteur Action Group 28 

B. Falzon, Imperial College London; GB 


Chair: TBD 


Attitude and Heading Reference System for an Integrated Stand-by Display Incorporating Solid State Sensors 

M. Carminati¹; G. Ferrari¹; M. Sampietro¹; R. Grassetti, Logic S.p.A., IT; ¹Politecnico di Milano, Dip. di Elettronica e 

Informazione, IT 


How to Avoid Contrail Cirrus 

H. Mannstein; K. Gierens; DLR, DE 


Aerodynamically Induced Formation of Contrails 

H. Mannstein; K. Gierens; B. Kärcher; B. Mayer; DLR, DE 


ECC Hall C Chair: TBD 

ECC Hall D 

Estrelsaal B 


Advanced GPS/INS Integration for Autonomous Mini and Micro Aerial Vehicle Navigation and Scientific Payload 

Applications 

A. Heindorf¹; T. Martin¹; M. Buschmann, Mavionics GmbH, DE; P. Vörsmann¹; ¹TU Braunschweig, DE 

38 


Improving runway safety through airborne traffic conflict detection and alerting 

D. Zammit-Mangion, Cranfield University, GB; A. Sammut¹; B. Zammit¹; ¹University of Malta, MT 


Enhancing the Dynamic System Simulation of an Aircraft Cabin Climate for Comfort-Improved Climate Control 

using 1D/3D Coupling 

H. Knigge, TUHH, DE; A. Joos, DE; G. Schmitz, DE 


Efficient Double Root Optimal Path Determination 

P.H. Richter, O & S Consultancy, DE 


Optimal Path Determination Observing Turn Restrictions 

P.H. Richter, O & S Consultancy, DE 


An e-Learning System for Polish Aviation Training Center 

P. Michalowski; P. Madrzycki; D. Karczmarz; Air Force Institute of Technology, PL 


Chair: TBD 


Trailing Edge Treatment to Enhance High Lift System Performance 

F.M. Catalano; G.L. Brand; R.C. Lemes; Aerodynamic Laboratory - University of Sao Paulo, BR 


In-House Integration of Space Payloads: CNES Facilities and Activities in Progress 

V. Dubourg; C. Escande; P. Agogue; O. Maes; CNES, FR 


Concept of an Autonomous Telepresence Module for Inter-Satellite Communication 

R. Lundin; E. Stoll; U. Walter; Lehrstuhl für Raumfahrttechnik, Technische Universität München, DE 

ECC Room 2 


FDMP - Concept of an Improved Flight Data Analysis Methodology 

H. Flühr¹; S. Sporer¹; G. Knoll¹; M. Haider¹; D. Reisinger, Austrian Airlines, AT; ¹FH JOANNEUM Graz, AT


Chair: TBD 


Resistance of Composite Tank Structures to the Hydraulic Ram Generated by the Impact and Penetration of a 

Ballistic Projectile 

J. Dupas; J. Fabis; J.M. Mortier; A. Deudon; ONERA, FR 


Stochastic Approach For The Sizing Of Space Launchers Components 

E. Gery, CNES, FR 


Optimization of Bolted Joints Connecting Honeycomb Panels 

G. Bianchi¹; G. S. Aglietti¹; G. Richardson, Surrey Satellites Technologies Ltd. (SSTL), GB; ¹University of Southampton, 

GB 


Biomechanics of the Cervical Spine and Helmet Mounted Display 

A. Guillaume, J. Lecompte, E. Chavary-Bernie, A. Laville, R. Portero, W. Skalli, S. Laporte, IMASSA, FR 


Chair: TBD 


Maintenance Credits, from the Monitoring of Helicopter Mechanical Parts to a Dynamic Maintenance Planning 

M.G Mathieu¹; J.-P. Derain¹; P.-l. Maisonneuve¹; S. Ghelam¹; P. Lyonnet, LTDS - ENISE, FR; ¹Eurocopter, FR 


Genetic Algorithm Optimization of Helicopter Blades Vibration Transition 

A. Gorjipoor, Sharif University of Technology, IR 


Application of Composite in next Generation of Airbus Long Range Aircraft especially in Fuselage Structures 

M. Kurzawa, Airbus Deutschland GmbH, DE 


Application of fibre metal laminates to aircraft structures 

F. Hashagen, Airbus Deutschland GmbH, DE 


ECC Room 3 

Chair: TBD 

ECC Room 1 

Room Paris 


SAND-MESH Plus - A Parameter Controlled Finite Element Pre-processor for Composite Sandwich Structures 

M. Streubig; K. Wolf; TU Dresden, Institute of Aerospace Engineering, DE 

39 


Study of Flowfield around Truncated Square Obstacle in Hypersonic Flow 

A. Ahmed; A. B. Ajmal Baig; S.B.H.S. Syed Bilal Hussain Shah; S.Z. Salimuddin Zahir; NESCOM, PK 


Design of Stable Fuzzy Controller for a Flight Based on Popov-Lyapunov’s Method 

Z.Q. Li; Y. Zhang; J. Deng; College of Aeronautics Northwestern Polytechnical University, CN 


Effects of Angle of Attack on a Swept-Back Wing 

S.C. Yen, National Taiwan Ocean University, TW 


Process-automation and Support of the Model-based Function Design for the IMA-Technology 

M. Lehmann, University Stuttgart, DE; E. Kleemann, Airbus-Germany, DE; A. Maier¹; K. Klaubert¹; M. Vernov¹; ¹ILS, 

University Stuttgart, DE 


Using of Artificial Neuron Network to Approximation Program Function, Operating of Launch Vehicle Flight 

O. Lukyanovych; O. Kirichenko; O. Ivanov; RPI Hartron-Arkos ltd, UAger, Austrian Airlines, AT; ¹FH JOANNEUM Graz, 

AT 


Chair: C. Sickinger, DLR Braunschweig, DE 


Comparison of Tensile Properties of Two NiCoCrA / YSZ Microlaminates Produced by EB-PVD 

J. Liang; G. GuoDong Shi; Center for Composite Materials, Harbin Institute of Technology, CN 


Cesic - A Mature SiC Composite Technology For Space Applications 

M.R. Kroedel, ECM, DE 


Fatigue Damage Simulation in Hybrid Titanium-PEEK /AS4 Composite Laminates 

P. Naghipour; J. Hausmann; M. Bartsch; H. Voggenreiter; DLR, DE 


A New Concept for Testing Fatigue and Damage Tolerance at Aerospace Structure 

B. Zapf, RUAG Aerospace Structures GmbH, DE 

Estrelsaal A 


Shock and Elastic Waves in Space Structures: Simulation, Attenuation and Usage for Monitoring 

C. Zauner¹; H. Baier¹; M. Reindl, KRP Mechatec, DE; ¹TU Muenchen, DE

Poster Session 9 Poster Session 10 

Chair: J. Block, DLR Braunschweig, DE Estrelsaal C1 Chair: M. Gädke, DLR Braunschweig, DE 

Estrelsaal C3 


System-Level Mass Savings from a Multifunctional Powerstructure 

S.C. Roberts; G.S. Aglietti; University of Southampton, GB 


The Effects of Microstructure on Cavity Nucleation and Propagation for UHTCs Used in HCV 

J. Liang, Harbin Institute of Technology, CN; C. Wang, Center for Composite Materials,Harbin Institute of Technology, CN 


Development of a Class of Shell Finite Elements for Nonlinear Applications 

R.G. Winkler, Unit of Engineering Mathematics, University of Innsbruck, AT 


Mechanical Behaviours and Fracture Mechanisms of Rigidifiable Composites for Inflatable Structures 

V. Calard, Austrian Research Centers GmbH, AT; B. Defoort, Astrium Space Transportation, FR; S. Langlois, 

ESA/ESTEC, NL 

40 


Prediction of the Pointing Stability from Ground Test and Its Initial In-orbit Evaluation of the Solar Observation 

Satellite SOLAR-B 

O. Takahara¹; K. Ichimoto, National Astronomical Observatory of Japan, JP; T. Shimizu, Institute of Space and 

Astronautical Science, Japan Aerospace Exploration Agency, JP; Y. Sakamoto, University of Tokyo, JP; S. Nagata, 

Kyoto University, JP; N. Yoshida¹; S. Shimada¹; ¹Mitsubishi Electric Corp., JP 


Robustness of Numerical Predictions of Clamp Band (C/B) Release Shocks 

J. Kasper, EADS Astrium GmbH, DE 


USV1 In-Flight Loads Evaluation by Means of Strain Gauge Instrumentation 

L. Di Palma; M. Belardo; M. Pecora; CIRA Scpa, IT 


Conception and Validation of a Two High Level Axes Set-up for Pyroshock Qualification of Space Electronic 

Equipments 

C. De Fruytier¹; F. Dell Orco¹; D. Wattiaux, Faculté Polytechnique de Mons, BE; ¹Thales Alenia SPace ETCA, BE

DGLR Short Course Aircraft Design, 11.-14. September 2007, Berlin, Germany 

TARGET DELEGATES 

The DGLR Short Course is arranged for graduated engineers, equivalent professionals and/or managers. 

It is likewise suitable for specialists in search of a broader perspective as for newcomers to the 

field. 

AIM 

The Short Course gives an insight into the procedures and the multidisciplinary interactions of aircraft 

conceptual design. The process of iterative synthesis and analysis in aircraft design is illustrated. A 

software tool for preliminary sizing is demonstrated. Methods and data to enable case studies of subsonic 

aircraft design are provided. 

CONTENT 

The Short Course Aircraft Design will cover following topics: 

Introduction 

Development Process 

Requirements 

Certification Standards 

Aircraft Configurations 

Engine Integration 

Preliminary Sizing 

Fuselage Design 

Wing Design (including High Lift) 

Empennage Design 

Prediction of Mass and CG-Location 

Landing Gear Design and Integration 

Drag Prediction 

Design Evaluation / DOC 

Military Aircraft Development 

LEARNING OBJECTIVES 

On completion of the Short Course, delegates will 

• know aircraft design parameters and methods 

• know the fundamental relationship of aircraft design parameters 

• be able to size and design an aircraft to the detail as covered during the Short Course 

• have a capability to structure aircraft design activities systematically and efficiently. 

VENUE 

Estrel Hotel, Berlin 

41

COURSE LEADER 

Prof. Dr.-Ing. Dieter Scholz, MSME, Department of Automotive and Aeronautical Engineering, Faculty 

of Engineering and Computer Science, Hamburg University of Applied Sciences and Leader of the 

DGLR Specialist Committee Manned Aircraft. 

http://www.ProfScholz.de. 

COURSE INSTRUCTORS (to be completed) 

Prof. Dipl-Ing. Erhard Rumpler (FH Munich), Prof. Dr.-Ing. Dieter Schmitt (TU Munich), Prof. Dr.-Ing 

Dieter Scholz (HAW Hamburg), Prof. Dr.-Ing. Jürgen Thorbeck (TU Berlin), Dipl.-Ing. Hannes G. Ross 

(TU Munich) 

Professor Erhard Rumpler 

Professor at FH Munich for construction design 

Prof. Dr.-Ing. Dieter Schmitt 

Nominated Professor (Ordinarius) at the Institute of Aerospace at the Technical University in Munich/Germany, 

(Chair for Aeronautical Engineering). Airbus Vice President „Research & Future Projects 

(retired) 

Prof. Dr.-Ing. Dieter Scholz, MSME 

Professor at Hamburg University of Applied Sciences. Teaching and leading research in the area of 

Aircraft Design, Flight Mechanics, Aircraft Systems 

Prof. Dr.-Ing. Jürgen Thorbeck 

Professor TU Berlin, Institute of Aeronautics and Astronautics; former Senior Manager Fleet Development 

Deutsche Lufthansa 

Dipl.-Ing. Hannes G. Ross 

TU Munich, Lecturer Advanced Design & Technology, Bundesakademie für Wehrtechnik und Verwaltung, 

Mannheim, Lecturer Military Aircraft development 

COSTS 

The costs for the DGLR Short Course will be 650 €, incl. 19% VAT. 

The fee includes coffee/tea and biscuits during the breaks, participation at the Parliamentary Evening 

on the Tuesday, 11 th , September and the Conference Dinner of the 1st European Air and Space Conference 

on Wednesday, 12 th, September. Registration Forms are available at 

www.ceas2007.org/ShortCourse/. 

CERTIFICATE 

After successful participation of the DGLR Short Course each delegate will receive a DGLR certificate 

signed by the president of the DGLR Prof. Dr.-Ing. Joachim Szodruch and Course Leader Prof. Dr.-Ing 

Dieter Scholz, MSME. 

42

General Information 

GENERAL 

The 1st CEAS European Air & Space Conference 

is hosted by the DGLR (German Society for 

Aeronautics and Astronautics) in conjunction with 

its annual national conference: Deutscher Luft– 

und Raumfahrtkongress 2007. In addition and 

only for this special occasion the biannual 

Conference on Spacecraft Structures, Materials 

and Mechanical Testing will be embedded in 

CEAS 2007 (www.ceas2007.org). 

The 1 st CEAS Conference will be held at the 

Estrel Convention Center (ECC) Berlin, Germany 

from Monday, 10 September to Thursday, 13 

September 2007. 

CONFERENCE LANGUAGE 

Conference language is English – presentations 

are preferred in English but also permitted in 

German. 

REGISTRATION FEES (EUROPEAN EURO €) 

Category 

Member 1 - early registration 2 450 € 

Member - normal and on-site 

registration 3 550 € 

Non-Member - early registration 580 € 

Non-Member - normal and on-site 

registration 680 € 

Student 4 Member - early registration 

Student Member normal and on-site 

90 € 


Student Non-Member - early Registration 

190 € 

Student Non-Member - normal and 

on-site registration 290 € 

Retired Member 5 early registration 

Retired Member normal and on-site 

190 € 


Accompanying Person 6 80 € 

For all prices VAT is included 

CONDITIONS 

1 

Members of any CEAS Member Society. 

2 

Early registration means including 31 July. 

3 

Normal registration means after 31 July. 

4 th 

Until completion of the 28 year. Reduction is 

not obtained for presenters. The student 

verification section of the registration MUST be 

completed and signed. Student registrations 

without this section completed will be returned to 

the applicant. 

5 Retired person and after completion of the 65 th 

year. 

6 Any accompanying person must be registered. 

Registration fee includes: 

Full Delegates – Attendance at the Congress 

sessions, coffee/tea during the breaks, Opening 

Ceremony on Monday Afternoon, Welcome 

Reception on Monday Evening by the Senate of 

Berlin, Parliamentary Evening on Tuesday, Final 

Programme, Proceedings on DVD, Congress bag 

and name badge. 

Students – Same as Full Delegates. 

Accompanying Persons – Attendance at 

Opening Ceremony on Monday Afternoon, 

Welcome Reception on Monday Evening, 

Parliamentary Evening on Tuesday Evening, 

Conference Dinner on Wednesday evening and 

the possibility to book organized Social 

Programme. 

REGISTRATION AND PAYMENT 

There are two ways of registration: 

1) Participants are required to complete the 

registration form in this programme*. 

machtWissen.de AG is responsible for all aspects 

concerning registration and payment. The 

complete registration form must be faxed or mailed 

directly to machtWissen.de. 

* An electronic version of the registration form is 

available on the website (www.CEAS2007.org). 

When using this form, it is appreciated if the 

registration form is downloaded and filled in by use 

of a PC. 

2) Online registration is possible on 

www.CEAS2007.org. If you choose this option, 

online payment by credit card is required. 

For further information, please contact: 

DGLR – Deutsche Gesellschaft für Luftund 

Raumfahrt Lilienthal-Oberth e.V. 

Mr. Peter Brandt 


D - 53175 Bonn 

Telephone: +49 (0) 228-30805-0 

Fax: +49 (0) 228-30805-24 

E-Mail: ceas@dglr.de 

For further information concerning registration 

and payment, please contact: 

43 

machtWissen.de AG 

Mr. Carsten Holze 

Fahrenheitstr. 1 

28359 Bremen 

Telephone: +49 (0) 421-2208-266 

Fax: + 49 (0) 421-2208-267 

E-mail: carsten.holze@machtwissen.de

METHODS OF PAYMENT 

Upon receiving your registration form, 

machtWissen.de will send you a confirmation. 

Your receipt is handed out at the congress 

registration desk (if an invoice is desired in 

advance, please contact machtWissen.de AG). 

Please choose and indicate one of the two 

methods of payment noted in this section. All 

payments must be in EURO. If you choose to pay 

by credit card, the full amount will be charged to 

your credit card prior to the congress date. 

Cheques are not accepted. 

Bank Transfer: 

Sparkasse Bremen 

Account name: machtWissen.de AG 

Account No: 1046853 

(IBAN DE49 290501010001046853) 

Bank Code: 29050101 

BIC/SWIFT code: SBREDE22 

Credit Card: 

American Express, Visa and Master Card are 

accepted. For those paying by credit card, the 

total cost for registration and tours will be charged 

to your credit card. 

REGISTRATION DESK 

The registration desk, situated in the rotunda, the 

pass way from the ECC to the Estrel Hotel, will be 

open during the following hours: 

Monday, 10. September 12:00 - 18:00 hrs 

Tuesday, 11. September - 

Wednesday, 12. September 07:30 - 18:00 hrs 

Thursday, 13. September 08:00 - 17:00 hrs 

TOUR RESERVATIONS 

ConTour GmbH has arranged the accompanying 

person´s programme listed on the following 

pages. Participants who wish to book these tours 

should complete the accompanying person´s 

programme section in the registration form. Tour 

reservations will be confirmed when tour charges 

are paid in full. Credit card payments for 

accompanying person’s tour charges will be 

deducted in full by machtWissen.de AG. 

HOTEL RESERVATIONS 

DGLR has reserved blocks of rooms at the hotels 

listed on the following pages from Monday, 10. 

September to Thursday, 13. September where 

rates have been especially negotiated for CEAS 

2007 delegates. 

Bookings will be taken on a first-come, firstserved 

basis. If the hotel of your request is fully 

booked, an alternative reservation has to be made 

at another hotel. You have to refer your hotel 

reservation directly to the desired hotel naming 

the KEYWORD “CEAS 2007”. 

Any hotel expenses are to be paid directly at the 

hotel by the guests themselves. 

BERLIN YOUTH HOSTEL 

To provide inexpensive accommodations for the 

Congress delegates and students of CEAS 2007 

we advise to search for Youth Hostels in Berlin. 

For reservation please contact directly the desired 

Youth hostel. 

CANCELLATION OF REGISTRATION, ETC. 

After you have received the confirmation notice 

from machtWissen.de AG, cancellation is subject 

to the following charges. Bank charges will be 

deducted from any refund. Notification of 

cancellation must be made to machtWissen.de 

AG. 

Registration fee 

Cancellations must be reported in writing to 

machtWissen.de AG. It must be received by 

1 August 2007 in which case registration fees will 

be refunded except for a cancellation fee of EUR 

40. In case the cancellation is received after 1 

August 2007, no refund would be given. 

This includes also the costs of the conference 

dinner. 

Accompanying Persons Programme 

Cancellations must be received by 1 August 2007 

in which case the tour fees will be refunded. In 

case the cancellation is received after 1 August 

2007, no refund would be given. 

CONGRESS PROCEEDINGS 

The CEAS 2007 Congress proceedings are 

available on CD-ROM, which are included in the 

registration fee where indicated. Additional CD- 

ROM can be ordered with the registration form at 

a cost of 90 EUR. 

For viewing the CD-ROM computers will be 

available in room 8 (Straßburg) on the ground floor 

at the ECC venue. If you require hard copies of 

single papers, they are available for purchase onsite 

(papers in the CD-ROM only). Orders are 

made at the registration desk at a cost of 2 EUR 

per paper (black & white copy only). Ordered hard 

copies will be available at the registration desk by 

the following morning. 

44

INTERNET ACCESS 

The DGLR has arranged an internet cafe with five 

PC-stations. The internet cafe is located on the 

ground floor of the ECC venue in room 8 

(Straßburg). Internet access is free of charge for 

registered persons. 

INSURANCE 

Participants are advised to take out their own 

travel insurance and to extend any private 

policies for personal possessions they may be 

bringing with them. The Congress does not cover 

participants against travel, cancellations or 

bookings or loss/theft of belongings. 

USEFUL HINTS 

ESTREL CONVENTION CENTER 

Berlin, the capital of Germany, is dynamic, 

cosmopolitan and creative, allowing for every kind 

of lifestyle. East meets West in the metropolis in 

the heart of a changing Europe. Germany’s 

largest city is a city of opportunities waiting to be 

sized in all areas, like entertainment, recreation, 

economy, science and academic life, as well as in 

politics. The Estrel Berlin is said to be Europe’s 

largest convention, entertainment and hotel 

complex. With 1,125 rooms and suites, five 

restaurants, two bars, a beer garden, the Estrel 

has plenty to offer to every guest. Beside the 

Estrel Hotel accommodation will be available in 

various prize categories. 

AIR TRAVEL AND ACCESS TO THE VENUE 

BY TAXI FROM THE AIRPORT 

Airport Tegel: The costs for a taxi taking you to 

the ECC venue are about 30 EUR and it takes 

approximatly 30 minutes. 

Airport Tempelhof: It takes approximately 10 

minutes and the costs are about 12 EUR. 

Airport Schönefeld: From this airport it takes 

approximately 20 minutes and the costs are about 

22 EUR. 

PUBLIC TRANSPORT FROM THE AIRPORT 

Airport Tegel: approximately 50 min, EUR 2, 10, 

(fare zone AB, ticket has to be stamped before 

entering or rather in the bus). Bus X9 or 109 until 

“Jungfernheide”, change to city train line 42 (circle 

line) until “Sonnenallee”. At Sonnenallee go 

approximately 80 meters to the left until you reach 

the Hotel. 

Airport Tempelhof: approximately 22 min, EUR 

2,10 (fare zone AB, ticket has to be stamped 

before entering or rather in the bus), undergroundstation 

“Platz der Luftbrücke” take line U6 

(destination Alt Mariendorf) until “Tempelhof”. 

Change to tramway line 42 (circle line) until 

“Sonnenallee”. At Sonnenallee go approximately 

80 meters to the left until you reach the Hotel. 

Airport Schönefeld: approximately 30 min, EUR 

2,10 (fare zone AB, ticket has to be stamped 

before entering or rather in the bus). Bus 171 until 

tramway station “Flughafen Berlin-Schönefeld”. 

Tramway line 9 until “Treptower Park”, transfer to 

line 41 (circle line) until “Sonnenallee”. At 

Sonnenallee go approximately 80 meters to the 

left until you reach the Hotel. 

BY CAR FROM THE AIRPORT 

Airport Tegel: 

Motorway 100/102, exit Grenzallee (approx. 30 

min.) 

Airport Tempelhof: 

Motorway 102, exit Grenzallee (approx. 10 min.) 

Airport Schönefeld: 

Exit B96a to crossroad Baumschulenstraße, then 

Sonnenallee (approx. 20 min.) 

FROM THE STATIONS 

Main station Berlin 

Bus No. M41 (until Ziegrastrasse) 

Eastern Station 

Tramway S5, S75 or S9 to Ostkreuz, transfer to 

S41 until “Sonnenallee”, at Sonnenallee go 

approximately 80 meters to the left until you reach 

the Hotel. 

PASSPORT AND VISA 

In Germany, everyone must have a valid identity 

card or passport. It is the responsibility of each 

delegate to obtain all the necessary documents, 

including visa if necessary. Participants requiring 

visas should apply to a German consular office or 

diplomatic mission in their respective country well 

in advance to departure. Participants are advised 

to contact their local travel agencies or airline 

companies for assistance. Details and an 

application form for Schengen Visa in several 

languages can be found on: 

45

http://www.auswaertiges-amt.de 

� “Willkommen in Deutschland” 

� „Überblick“ 

� „Einreisebstimmungen“ 

If you need any assistance for visa acquisition 

(like a special invitation letter) after you have 

contacted your local travel agencies or airline 

companies, please feel free to contact the DGLR 

Office. Timely visa acquisition should be not later 

than 30 June 2007. 

Currency 

DGLR – Deutsche Gesellschaft für 

Luft- und Raumfahrt 

Lilienthal-Oberth e.V. 


D-53175 Bonn 

Phone: (+49) 228-3 08 05 10 

Fax: (+49) 228-3 08 05 24 

e-mail: ceas@dglr.de 

http://www.DGLR.de 

The currency used in Germany is European 

EURO (EUR, €). Notes are available in units of 

EUR 5, 10, 20, 50, 100, 200, and coins in units of 

Cent 1, 2, 5, 10, 20, 50 and EUR 1 and 2. 

Traveler´s checks and currencies from most 

countries can be exchanged for European EUR at 

major banks and hotels. Only European EUR is 

accepted at regular stores and restaurants. 

Credit Cards 

International credit cards such as Master Card, 

Visa, American Express and Diners Club are 

widely accepted at hotels, department stores, 

large shops and restaurants. 

Tax and Tipping 

In Germany there is the custom of paying 10 

percent of the amount of the bill as tipping in 

restaurants. A 19% sales tax applies to almost all 

consumer goods sold in Germany. 

Climate 

Berlin is located in between the changeover of 

oceanic and continental dominated climate. In the 

month of September the average daytime 

temperature in Berlin a comfortable 65°F (18° C). 

The average number of rainy days is 14 and days 

of sun 5,2. Participants are therefore 

recommended to bring normal summer clothing 

with adequate clothings for cooler and rainy days 

and evenings. 

Electricity 

220-230 volts AC, 50-60 Hz 

Business Hours 

Bank Mo + Thu 9:00 – 13:00 / 14:00 – 18:00 

Tue + Wed 9:00 – 13:00 / 14:00 – 16:00 

Fri 9:00 – 13:00 

Closed on weekends and holidays 

Post Office 

Mo – Fri 8:00 – 18:00 

Sa 8:00 – 12:00 

Shops 10:00 – 20:00 (typical time) 

Restaurants 11:00 – 23:00 (typical time) 

Time 

CET with daylight saving time at this period. 

Mobil phones 

For the use of mobile phones in Berlin, Germany, 

they must be designed for the GSM frequencybands 

900 MHz or 1800 MHz. Additionally the use 

of UMTS mobile phones in the area of the venue 

is possible but there is no coverage guaranteed all 

over Germany. 

46

Social Programme 

Monday 10 September Congress Reception by the Senate 

19:00 - 21:30 hrs 

(login in registration form is necessary to receive ticket, included in Delegate, Student and 

Accompanying Person´s fee) 

Delegates, Students and Accompanying Persons are invited to attend the Congress Reception in the 

Town Hall. A bus shuttle from the Estrel to the Town hall is organised (start of transfer 18:30). 

Complimentary light snacks and drinks will be served. 

Tuesday 11 September Parliamentary Evening 

19:00 

(login in registration form is necessary to receive ticket, included in Delegate, Student and 

Accompanying Person´s fee) 

Delegates, Students and Accompanying Persons are invited to attend the Parliamentary Evening in 

the Estrel Convention Hall A. 

Wednesday 12 September Conference Dinner 

19:30 - 24:00 hrs 55 € per person 

(included in Accompanying Person´s fee) 

The Congress Banquet will be held in the pleasing Hall A of the Estrel Convention Center. The Dinner 

will serve a buffet-type dinner including beverage (except for hard liquors) until 24:00. Guests must 

present purchased tickets for entry. 

Accompanying Persons Programme 

(subject to minimum numbers of participants, english speaking guides) 

TUESDAY, 11 SEPTEMBER 

10:00 – 13:00 hrs 

Big Berlin Tour 

Highlights of the capital with the Government area 

20 € per person 

In the morning a bus will be waiting for you in front of the Estrel hotel. Sitting in a comfortable seat, you 

will start to discover the capital. This bus tour with English and German speaking guides will give you 

an overview of the well known sights of Berlin: Kaiser-Wilhelm-Memorial Church, Europe Centre, 

Bauhaus Museum, New National Gallery, Philharmonic Hall, Potsdamer Platz/Sony Centre, Jewish 

Museum, Checkpoint Charlie – Wall Museum, Gendarmenmarkt, Alexanderplatz, St.-Nicolai Quarter, 

City Hall of Berlin, TV-Tower, Berliner Dom, Zeughaus, State Opera, Boulevard Unter den Linden, 

Brandenburger Tor, Holocaust memorial, Berlin central station, Reichstag, Government Area 

Chancellery, Tiergarten, Bellevue Palace, Siegessäule, Charlottenburg Palace, Olympic Stadium, 

Grunewald Forest, Radio Tower, ICC, Kurfürstendamm and more. 

After this bus tour you will have the opportunity to have lunch in a nice little restaurant at the 

Gendarmenmarkt (not included in the tour fee). 

14:30 – 17:30 hrs 

Historical Berlin Walk including a trip to the Pergamon Museum 


Our afternoon´s programme offers a walking tour through the history of Berlin. Meeting Point is the 

Gendarmenmarkt, starting from the there, you will discover the capital where it is most beautiful: 

between Gendarmenmarkt, St.-Nikolai Quarter and Schloßplatz, Boulevard Unter den Linden and 

47

Friedrichstraße. An English and German speaking guide will report about the foundation of Berlin in 

the 13th century and its development to one of Europe’s most exciting capitals. Here, in Berlin Mitte, 

many great kings of the past have left their marks on the metropolis. 

The tour will end on the Museumsinsel (museum island). There you will have the opportunity to visit 

the world-famous Pergamon Museum (included in the tour fee). 

WEDNESDAY, 12 SEPTEMBER 

10:00 – 16:00 hrs 

Guided tour to Potsdam / Sanssouci - including Palace of Sanssouci 


The former Royal City of Potsdam, an UNESCO world heritage site with its unique collection of 

palaces and parks, is located just an hour away from the centre of Berlin. The rococo Palace of 

Sanssouci became the favourite refuge of Prussia’s greatest King, Friedrich II. Here, the Philosopher 

of Sanssouci entertained some of the most educated men of his time, among them the French poet 

Voltaire who was a frequent guest over many years. 

Our excursion - starting from Estrel Hotel - takes you on an extensive tour of Sanssouci Palace with a 

stroll through the magnificent gardens, and a city tour of Potsdam during which you discover the heart 

of the baroque city with its Dutch Quarter and Russian Colony Alexandrovka. A lunch break in 

Potsdam is included. The bus tour ends again at the Estrel Hotel. 

THURSDAY, 13 SEPTEMBER 

9:30 – 13:00 hrs 

Berlin from the water site - River Cruise on Landwehrkanal and Spree 


We invite you to a special event – a beautiful boat trip through the water ways of the capital. 

Experience the variety of architectural styles on our city cruise and discover that Berlin has more 

bridges than Venice. You will see Oberbaum Brücke, Oberschleuse, Science Museum, Charlottenburg 

Palace, Spreebogen, Bellevue Palace, Government Quarter, Reichstag (Seat of the German 

Government), Charité, Museum Island, Berliner Dom, St.- Nikolai Quarter, Palast der Republik and 

more. On board, you will have the opportunity for having lunch (not included in the tour fee). 

The boat trip will finally take you to the well-known Friedrichstraße. Here, you can go on your own 

individual shopping tour or join us in the afternoon`s programme: a guided tour to the famous 

Kaufhaus des Westens (KaDeWe) at the Boulevard Kurfürstendamm. 

14:00 – 16:00 hrs 

The famous KaDeWe (Kaufhaus des Westens) – a guided tour through 

the Palace of Shopping 


The Kaufhaus des Westens (Department store of the West, commonly abbreviated KaDeWe) is a 

department store in Berlin and the second largest in all of continental Europe. 

Its sheer size, large selection and fame for excellent quality as well as its central location in the heart 

of Berlin at the famous Boulevard Kurfürstendamm makes it a must for every tourist visiting Berlin. 

On this tour, we would meet at 14:00 h at the Information Point on the groundfloor in the entrance hall 

of the KaDeWe, directly behind the main entrance. The 5,00 € fee has to be paid on-site and will be 

given back to you in the form of a coupon (“Wunschkarte”). 

48

Technical Tours Friday 14 September 

Following Technical Tours at a cost of 10 Euro per person are possible to attend for Full Delegates 

and Students (subject to availability) – due to the limited capacity, reservations will be taken on a firstcome, 

first served basis. A refund of the cost sharing is not possible. Only registered persons can 

participate these tours. 

These technical tours have been arranged by the DGLR. The tours include coach transfers. 

Please indicate your preference in the registration form. 

A: 

10:00 – 16:00 hrs 

Participants will visit Kummersdorf with its historical missiles - after that you will have the opportunity 

to see the construction site of the airport Schönefeld. 

B: 

10:00 – 15:00 hrs 

Participants will visit Berlin-Gatow and the Air Force Museum, the way back leads through the Airport 

Berlin Tegel. 

C: 

Participants will visit the construction site of the airport Schönefeld. 

10:00 –13:00 hrs 

D: 

10:00 – 14:00 hrs 

Participants will visit Berlin-Adlershof (DLR) with its planet research and satellites, after that they will 

see the historical examination ground (GBSL). 

E: 

10:00 – 13:00 hrs 

Participants will visit the Technical University of Berlin and have the opportunity to see the flight 

simulator A330. 

F: 

10:00 – 16:00 hrs 

Participants will visit Stölln, the place of death during a flight experiment of Lilienthal Fliegeberg and 

they will also see the inauguration of the Lilienthal memorial. 

G: 

10:00 – 16:00 hrs 

Participants will visit the museum of transportation and technics with its exhibition of aeronautics and 

astronautics. 

49

Choice of pre-reserved Hotels 

Hotel reservation by use of the KEYWORD “CEAS 2007”, prices are inclusive breakfast (except for 

Estrel and Ellington, see table below) 

Hotel 

Estrel Hotel Berlin**** 

Sonnenallee 225, 12057 Berlin 

Phone: +49 30 - 6831 - 0 

Fax: +49 30 - 6831 - 2345 

E-Mail: hotel@estrel.com 

Special conditions available until 9 th August 

2007 

Ellington Hotel Berlin (designer hotel) 

Nürnberger Str. 50-55, 10789 Berlin 

Phone: +49 30 - 6831 - 52 303 

Fax: +49 30 - 6831 - 55 555 

E-Mail: contact@ellington-hotel.com 

Special conditions available until 9 th August 

2007 

Park Hotel Blubb**** 

Buschkrugallee 60 – 62, 12359 Berlin 

Phone: +49 30 - 600 03 716 

Fax: +49 30 - 600 03 777 

E-Mail: reservierung@park-hotel-blub.de 

Special conditions available until 16th July 2007 

Best Western Euro-Hotel Berlin***+ 

Sonnenallee 6, 12047 Berlin 

Phone: +49 30 - 61 382-0 

Fax: +49 30 - 61 382 - 222 

E-Mail: info@euro-hotel.net 


Best Western Hotel Ravel **** 

Rudower Str. 80 - 82, 12351 Berlin 

Phone: +49 30 - 666 80 - 0 

Fax: +49 30 - 666 80 - 800 

E-Mail: verkauf@ravel.bestwestern.de 


Tulip Inn Berlin-Friedrichshain***+ 

Gürtelstraße 41, 10247 Berlin 

Phone: +49 30 - 29 383 - 0 

Fax: +49 30 - 29 383 - 222 

E-Mail: info@tulip-inn-berlin.com 


A&O Hostel** 

Köpenicker Str. 127 – 129, 10179 Berlin 

Phone: +49 30 – 80 947 – 14 

Fax: + 49 30 – 80 947 – 20 

E-Mail: booking@aohostels.com 


Venue 

Distance 

7 km 

public transport 

available / bus 

shuttle against 

cost sharing is 

available 

2,8 km, 


available 

3,5 km 


available 

5 km 


available 

8 km 


available 

7 km 


available 

50 

Single / € 

110,00 

(excl. breakfast, 

15,50 € pP) 

if avail. Deluxe 

135,00 

(excl. Breakf. 

15,50 € pP) 

16- 20 m 2 

65,00 

20-25 m 2 

80,00 

25-30 m 2 

90,00 

79,00 

Double / € 

121,00 

(excl. breakfast, 

15,50 € pP) 

if avail.Deluxe 

146,00 

(excl. Breakfast, 

15,50 € pP 

16- 20 m2 

75,00 

20-25 m2 

90,00 

25-30 m2 

100,00 

90,00 

79,00 99,00 

one night 

85,00 

from two nights 

79,00 

105,00 

98,00 

70,00 90,00 

58,31 73,78

www.CEAS2007.org 

is supported by 

CEAS@DGLR.DE

Deutscher Luft- und Raumfahrtkongress 2007 - CEAS 2007

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