30.10.2012 Views

lisa pathfinder All the space you need - Astrium - Eads

lisa pathfinder All the space you need - Astrium - Eads

lisa pathfinder All the space you need - Astrium - Eads

SHOW MORE
SHOW LESS

You also want an ePaper? Increase the reach of your titles

YUMPU automatically turns print PDFs into web optimized ePapers that Google loves.

<strong>lisa</strong><br />

<strong>All</strong> <strong>the</strong> <strong>space</strong> <strong>you</strong> <strong>need</strong><br />

<strong>lisa</strong> <strong>pathfinder</strong><br />

The LISA Pathfinder mission is a technology demonstrator mission that will test a series of ultra-high<br />

precision technologies to be used on a later, and much larger, international project LISA (Laser Interferometric<br />

Space Antenna), for which <strong>the</strong> European Space Agency is preparing a leading European role.<br />

LISA Pathfinder will carry out in-orbit testing of <strong>the</strong>se key technologies including <strong>the</strong> micro-propulsion systems,<br />

<strong>the</strong> drag-free control systems and <strong>the</strong> technologies associated with <strong>the</strong> payload. There are two payload test<br />

packages, one from ESA funded by national institutes and universities and drawn toge<strong>the</strong>r under <strong>the</strong> auspices<br />

of <strong>Astrium</strong> GmbH as <strong>the</strong> LTP architect, whilst <strong>the</strong> second payload is provided by NASA.<br />

The primary LISA mission will measure gravitational waves generated by exotic cosmic events such as collapsing<br />

binary star systems and <strong>the</strong> collision of massive black holes. Through LISA Pathfinder, EADS <strong>Astrium</strong> will<br />

augment its proven capability in astronomy and planetary exploration by development of <strong>the</strong> know-how for<br />

<strong>space</strong>-based fundamental physics exploration.


7321tl oct 08 © <strong>Astrium</strong>, images © <strong>Astrium</strong><br />

Customer European Space Agency<br />

Mission Technology demonstration for <strong>the</strong> future LISA mission – to detect relative<br />

movement of two solid bodies freely floating in <strong>space</strong> with accuracy of<br />

10 picometers<br />

Orbit 500 000 x 800 000km Halo orbit around L1<br />

Spacecraft • Spacecraft mass: 450kg<br />

• Propulsion module including fuel: 1420kg<br />

Payload • The LISA Test Package (LTP)<br />

• The Disturbance Reduction System (DRS) from JPL/NASA<br />

Features 2 gold platinum cubes of 46mm<br />

NASA JPL CFE. Measurement of SL position @ millionth of mm.<br />

Launch Mass 1910kg<br />

Dimensions 2.7m high by 2.1m diameter<br />

Launch Date 2011<br />

Mission Duration After calibration at <strong>the</strong> L1 position, <strong>the</strong> in-flight demonstration of <strong>the</strong> LISA<br />

technology will take 90 days for <strong>the</strong> LTP and 85 days for <strong>the</strong> DRS<br />

Status Implementation started Feb 2004<br />

Development started Feb 2006<br />

<strong>Astrium</strong> Responsibilities • Prime contractor<br />

• System and platform design and build<br />

• Drag-Free Attitude Control System (DFACS)<br />

• LISA Test Package (LTP) industrial lead (separate ESA contract)<br />

Key Features:<br />

drag-free and attitude Control system<br />

The mission objective is to verify that a test mass can be kept on-board <strong>the</strong> <strong>space</strong>craft “free-floating” to<br />

within 3x10 -14 ms -2 , this means that <strong>the</strong>re must be no mechanical contact and <strong>the</strong> electrical, magnetic, <strong>the</strong>rmal<br />

and gravitational internal forces must be below 3x10 -14 ms -2 . To achieve this, <strong>the</strong> position and rotation of <strong>the</strong><br />

test mass is monitored and <strong>the</strong> attitude control system calculates <strong>the</strong> necessary forces and torques to apply<br />

to <strong>the</strong> <strong>space</strong>craft to maintain a steady position and orientation of <strong>the</strong> test mass within its housing. Even <strong>the</strong><br />

pressure of <strong>the</strong> solar wind must be compensated for.<br />

<strong>lisa</strong> test paCkage<br />

The LTP represents one arm of <strong>the</strong> LISA interferometer, in which <strong>the</strong> distance between <strong>the</strong> two test masses<br />

is reduced from 5 million kilometres to 35 centimetres. The LTP drag-free control system consists of an inertial<br />

sensor, a proportional micro-propulsion system and a control loop. The two identical 46mm cube test masses<br />

are housed in individual vacuum cans. The displacement of <strong>the</strong> cubes with respect to <strong>the</strong>ir housing is measured<br />

by capacitive sensing in three dimensions. These position signals are used in a feedback loop to command<br />

proportional micro-propulsion thrusters to enable <strong>the</strong> <strong>space</strong>craft to remain centred on <strong>the</strong> proof mass. Field<br />

Emission Electric Propulsion (FEEP) thrusters will be used as actuators.<br />

drs<br />

The DRS is a NASA supplied instrument. The DRS will use <strong>the</strong> sensor information of <strong>the</strong> LTP (test masses<br />

position and attitude) to control <strong>the</strong> <strong>space</strong>craft attitude with independent drag-free software and will use<br />

colloidal thrusters as actuators.<br />

For more information please contact:<br />

Elizabeth Seward, Marketing Manager<br />

Earth Observation & Science Division<br />

astrium satellites<br />

Gunnels Wood Road<br />

Stevenage<br />

Hertfordshire<br />

SG1 2AS<br />

United Kingdom<br />

PHONE: +44 (0) 1438 778060<br />

FAX: +44 (0) 1438 778910<br />

EMAIL: elizabeth.seward@astrium.eads.net www.astrium.eads.net<br />

<strong>lisa</strong> <strong>pathfinder</strong> science structure equipped with<br />

mass dummies<br />

industrial team<br />

aBsl (aea)<br />

astrium<br />

scisys<br />

honeywell<br />

ssBV<br />

oerlikon<br />

saaB<br />

Crisa<br />

eads Casa<br />

rymsa<br />

teChnologiCa<br />

dnV<br />

patria<br />

fmi<br />

thales alenia <strong>space</strong><br />

galileo avionica<br />

alta<br />

astrium<br />

Zarm<br />

rWe<br />

thales alenia <strong>space</strong><br />

astrium<br />

terma<br />

alcatel alenia etCa<br />

spaCeBel<br />

austrian aero<strong>space</strong><br />

siemens<br />

arCs<br />

Critical software

Hooray! Your file is uploaded and ready to be published.

Saved successfully!

Ooh no, something went wrong!