Unmanned Aircraft Systems Roadmap 2005-2030 - Federation of ...

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UAS ROADMAP 2005 2.3.2 Maverick User Service: DARPA/Army/Navy Manufacturer: Boeing/Frontier/Robinson Inventory: 4 Delivered/5 Planned Background: Maverick is an unmanned version of the Robinson R22 helicopter. Frontier modified it in 1999 to serve as a testbed for developing the control logic for their DARPA A-160 UA effort. Subsequently, the Navy decided to acquire four Mavericks in 2003. Characteristics: Maverick Maverick Length 28.8 ft Rotorspan 25.2 ft Gross Weight 1,370 lb Payload Capacity 400 lb Fuel Capacity 100 lb Fuel Type AVGAS Engine Make Lycoming 0-360-J2A Power 145 hp Data Link(s) TBD Frequency TBD Performance: Endurance 7 hr Max/Loiter Speeds 118/0 kt Ceiling 10,800 ft Radius 175 nm Takeoff Means Hover Landing Means Hover Sensor EO/IR Sensor Make Wescam SECTION 2 - CURRENT UA PROGRAMS Page 21
UAS ROADMAP 2005 2.3.3 XPV-1 Tern User Service: SOCOM Manufacturer: BAI Aerosystems Inventory: 65 Delivered/65 Planned Background: Originally an Army testbed for a fiber-optic guided UA, Tern was completely retooled in late 2001 to give it a larger, steerable nose gear and main gear fitted with tires suitable for rough terrain with electronically-actuated disc brakes to aid short-field recovery that enabled the aircraft to carry a belly-mounted dispensing mechanism. Tern was operated in support of Special Operations Forces by Navy personnel from Fleet Composite Squadron Six (VC-6, previously the USN's Pioneer UA Squadron) in Afghanistan to perform force protection missions and to dispense an unattended ground sensor weighing over 20 pound. Over 225 combat hours were flown during two 3-month long deployments. In early 2004, a Tern variant was developed that eliminated the landing gear and incorporated skids and a tail-hook. A marinized control station was developed, and the system was successfully demonstrated onboard a Navy LPD (USS Denver). The reduced drag of the skid/tailhook recovery system improved the vehicle's mission endurance from 4 to over 6 hours. Characteristics: XPV-1 XPV-1 Length 9.0 ft Wing Span 11.4 ft Gross Weight 130 lb Payload Capacity 25 lb Fuel Capacity 28 lb Fuel Type MOGAS/oil Engine Make 3W 100 cc Power 12 hp Data Link(s) LOS C2 Frequency L/S-band LOS Video UHF Performance: Endurance 2 hr Max/Loiter Speeds 87/50 kt Ceiling 10,000 ft Radius 40 nm Takeoff Means Runway Landing Means Runway Sensor EO or IR Sensor Make BAI PTZ SECTION 2 - CURRENT UA PROGRAMS Page 22
Page 2 and 3: UAS ROADMAP 2005
Page 4 and 5: UAS ROADMAP 2005 EXECUTIVE SUMMARY
Page 6 and 7: UAS ROADMAP 2005 TABLE OF CONTENTS
Page 8 and 9: UAS ROADMAP 2005 FIGURE F-2: U.S. M
Page 10 and 11: UAS ROADMAP 2005 CBP Customs and Bo
Page 12 and 13: UAS ROADMAP 2005 ID Identification
Page 14 and 15: UAS ROADMAP 2005 1.0 INTRODUCTION 1
Page 16 and 17: UAS ROADMAP 2005 2.0 CURRENT UAS Th
Page 18 and 19: UAS ROADMAP 2005 2.1.2 RQ-2B Pionee
Page 20 and 21: UAS ROADMAP 2005 2.1.4 RQ-5A/MQ-5B
Page 22 and 23: UAS ROADMAP 2005 2.1.6 RQ-8A/B Fire
Page 24 and 25: UAS ROADMAP 2005 2.1.8 Joint Unmann
Page 26 and 27: UAS ROADMAP 2005 2.1.10 I-Gnat-ER U
Page 28 and 29: UAS ROADMAP 2005 2.1.13 Extended Ra
Page 30 and 31: UAS ROADMAP 2005 2.2.3 Cormorant Us
Page 32 and 33: UAS ROADMAP 2005 2.2.7 Eagle Eye Us
Page 36 and 37: UAS ROADMAP 2005 2.3.4 XPV-2 Mako U
Page 38 and 39: UAS ROADMAP 2005 2.3.6 Onyx Autonom
Page 40 and 41: UAS ROADMAP 2005 FQM-151 Pointer Ba
Page 42 and 43: UAS ROADMAP 2005 2.4.2 Micro Air Ve
Page 44 and 45: UAS ROADMAP 2005 launched and contr
Page 46 and 47: UAS ROADMAP 2005 2.5.2 Tethered Aer
Page 48 and 49: UAS ROADMAP 2005 2.5.6 High Altitud
Page 50 and 51: UAS ROADMAP 2005 2.6 UAS PROGRAMMAT
Page 52 and 53: UAS ROADMAP 2005 TABLE 2.7-1. CLASS
Page 54 and 55: UAS ROADMAP 2005 3.0 REQUIREMENTS R
Page 56 and 57: UAS ROADMAP 2005 TABLE 3.3-1. COMBA
Page 58 and 59: UAS ROADMAP 2005 3.5 INTEROPERABILI
Page 60 and 61: UAS ROADMAP 2005 4.0 TECHNOLOGIES U
Page 62 and 63: UAS ROADMAP 2005 over present compu
Page 64 and 65: UAS ROADMAP 2005 provide coverage t
Page 66 and 67: UAS ROADMAP 2005 recognized today a
Page 68 and 69: UAS ROADMAP 2005 Class A or B Misha
Page 70 and 71: UAS ROADMAP 2005 Weight, Lb 100,000
Page 72 and 73: UAS ROADMAP 2005 Panchromatic Calen
Page 74 and 75: UAS ROADMAP 2005 4.4.2 Communicatio
Page 76 and 77: UAS ROADMAP 2005 5.0 OPERATIONS 5.1
Page 78 and 79: UAS ROADMAP 2005 labs have been inv
Page 80 and 81: UAS ROADMAP 2005 5.3 OPERATIONS 5.3
Page 82 and 83: UAS ROADMAP 2005 5.3.3 battlespace
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UAS ROADMAP 2005 6.0 ROADMAP This S
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UAS ROADMAP 2005 range/endurance ai
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UAS ROADMAP 2005 level below that a
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UAS ROADMAP 2005 � Unmanned syste
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UAS ROADMAP 2005 Appendices
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UAS ROADMAP 2005 APPENDIX A: MISSIO
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UAS ROADMAP 2005 be treated more li
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UAS ROADMAP 2005 3. The integration
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UAS ROADMAP 2005 of expendables. In
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UAS ROADMAP 2005 Range Transporter
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UAS ROADMAP 2005 APPENDIX B: SENSOR
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UAS ROADMAP 2005 film can. Primary
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UAS ROADMAP 2005 mature, and integr
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UAS ROADMAP 2005 should be encourag
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UAS ROADMAP 2005 Contractors have p
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UAS ROADMAP 2005 APPENDIX C: COMMUN
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UAS ROADMAP 2005 FIGURE C-1. GLOBAL
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UAS ROADMAP 2005 GCS, Ops Cell MOB
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UAS ROADMAP 2005 (TSAT), Net-Centri
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UAS ROADMAP 2005 Architecture, GIG,
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UAS ROADMAP 2005 Tier 1 Team Covera
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UAS ROADMAP 2005 FIGURE C-7. BLACK
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UAS ROADMAP 2005 � Aircraft Contr
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UAS ROADMAP 2005 � Any new federa
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UAS ROADMAP 2005 communications, pr
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UAS ROADMAP 2005 CDL requirements e
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UAS ROADMAP 2005 decryption and enc
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UAS ROADMAP 2005 APPENDIX D: TECHNO
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UAS ROADMAP 2005 specific fuel cons
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UAS ROADMAP 2005 technology program
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UAS ROADMAP 2005 the effect of smal
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UAS ROADMAP 2005 Displays that show
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UAS ROADMAP 2005 29 % ($747.3 M) in
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UAS ROADMAP 2005 Laboratory Initiat
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UAS ROADMAP 2005 APPENDIX E: INTERO
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UAS ROADMAP 2005 layer 4 protocol i
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UAS ROADMAP 2005 The family of stan
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UAS ROADMAP 2005 Military Satellite
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UAS ROADMAP 2005 DoD Discovery Meta
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UAS ROADMAP 2005 STANAG 3809 (Digit
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UAS ROADMAP 2005 � SDN.706, X.509
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UAS ROADMAP 2005 Level 1: Indirect
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UAS ROADMAP 2005 APPENDIX F: AIRSPA
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UAS ROADMAP 2005 Class A or B Misha
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UAS ROADMAP 2005 Hawk and Predator,
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UAS ROADMAP 2005 knowledge skills r
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UAS ROADMAP 2005 decision and the a
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UAS ROADMAP 2005 OSD ROADMAP GOALS
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UAS ROADMAP 2005 APPENDIX G: TASK,
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UAS ROADMAP 2005 APPENDIX H: RELIAB
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UAS ROADMAP 2005 throughout its ACT
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UAS ROADMAP 2005 17% 14% 12% 19% 38
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UAS ROADMAP 2005 that for a number
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UAS ROADMAP 2005 RECOMMENDATIONS Ba
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UAS ROADMAP 2005 APPENDIX I: HOMELA
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UAS ROADMAP 2005 CUSTOMS AND BORDER
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UAS ROADMAP 2005 APPENDIX J: UNMANN
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UAS ROADMAP 2005 Joint Robotics Pro
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UAS ROADMAP 2005 Anti-Personnel/Obs
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UAS ROADMAP 2005 The UGV family wil
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UAS ROADMAP 2005 In Phase I, an exp
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UAS ROADMAP 2005 is NSWC Panama Cit
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UAS ROADMAP 2005 APPENDIX K: SURVIV
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UAS ROADMAP 2005 such as flares, ch
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UAS ROADMAP 2005 TABLE K-1. SURVIVA
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