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WASWFOVWSMRYYPGWide Area SensorWide Area Field of ViewWhite Sands Missile RangeYuma Proving GroundC-7
Appendix D – References1. The Senate Report accompanying S.1253 (S.Rept.112-26) of the National DefenseAuthorization Act for Fiscal Year 2012.2. Briefing – “DoD Lighter-Than-Air and Hybrid Aircraft Programs”, June 23, 2009. Overviewfor SAC-D Staff by USAF representatives.3. “Balloons and Airships”. Florida International University webpage. Updated November 2,2009. http://www.allstar. fiu.edu/aero/balloon5.htm.4. Recent Development Efforts for Military Airships. Congress of the United StatesCongressional Budget Office. Washington D.C: CBO, 2011.5. Airships and Balloons in the World War II Period. Judy Rumerman. US Centennial of FlightCommission. http://www.centennialofflight.gov/essay/Lighter_than_air/Airships_in_WWII/LTA10.htm.6. Bolkcom, Christopher—Specialist in National Defense Foreign Affairs, Defense, and TradeDivision. Potential Military Use of Airships and Aerostats CRS Report for Congress.7. Tethered Aerostat Radar System, U.S. Air Force Fact Sheet. Obtained fromhttp://www.af.mil/information/factsheets/factsheet.asp?fsID=35078. “Iraqi Conflict Brings Increased Interest in Military Airships.” Navy League of the UnitedStates. July 2003. Available at http://www.navyleague.org/sea_power/jul_03_01.php9. Directory of U.S. Military Rockets and Missiles, Appendix 4: Undesignated Vehicles. Lastupdated September 13, 2005. Available online at http://www.designationsystems.net/dusrm/app4/aerostats.html10. Image provided by PTDS PM Office.11. Report to Congress—Aerostats and Hybrid Airship Review. Office of the Under Secretary ofDefense for Acquisition, Technology, & Logistics. March 1, 2011.12. Briefing for Headquarters U.S. Air Force. “USAF Airship S&T” by representative ofSAF/AQR (Science, Technology, and Engineering) 29-Jul-2010.13. Briefing for Assistant Secretary of Defense for Research and Engineering, “HybridAirships.” July 19, 2011.14. Information provided through interview with representative from Persistent Surveillance, DAG-2 Intelligence Futures Directorate.15. Image provided by SMDBL ATB Office.16. “High-Altitude Test Bed (HATB) Support to the Network Integration Evaluation”Information Paper prepared by Army SMDC-FWB. May 18, 2011.17. Information provided through interview with representative from Army SMDC.18. Images provided by manufacturer, Silicis Technologies, Inc. Information provided throughinterview with representative from Army REF.D-1
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SUMMARY REPORT OF DoD FUNDED LIGHTE
Page 3 and 4:
TABLE OF CONTENTSEXECUTIVE SUMMARY
Page 5 and 6:
Figure 11: Computer Rendering of Al
Page 7 and 8:
Table 22: HALE-D Program Overview .
Page 9 and 10:
EXECUTIVE SUMMARYIn the Senate repo
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for unmanned aerial vehicle and cru
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Integrated Sensor Is Structure (ISI
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PREFACECongress, through the Senate
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PURPOSEThe purpose of this document
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INTRODUCTIONBackgroundModern LTA cr
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ground, large aerostats are anchore
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AirliftAirships, particularly hybri
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AEROSTAT PROGRAMSAerostats are air
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Aerostat Test Bed (ATB)Table 2: ATB
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AltusTable 4: Altus Program Overvie
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would otherwise lack organic survei
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Table 7: JLENS Technical Specificat
Page 35 and 36: Persistent Ground Surveillance Syst
Page 37 and 38: and advance systems capabilities as
Page 39 and 40: Length: 117 ft.Width: 39 ft.Height:
Page 41 and 42: Rapid Aerostat Initial Deployment (
Page 43 and 44: Rapidly Elevated Aerostat Platforms
Page 45 and 46: tether lengths to support different
Page 47 and 48: Length: 26.87 ft.Table 17: STMPAS T
Page 49 and 50: Table 19: TARS Technical Specificat
Page 51 and 52: AIRSHIP PROGRAMSDespite the fact th
Page 53 and 54: Figure 30: Size Comparison for Hybr
Page 55 and 56: Table 21: Blue Devil 2 Technical Sp
Page 57 and 58: High-Altitude Long Endurance-Demons
Page 59 and 60: HiSentinelTable 24: HiSentinel Prog
Page 61 and 62: Table 26: Comparison of HiSentinel
Page 63 and 64: Table 28: ISIS Technical Specificat
Page 65 and 66: Table 30: LEMV Technical Specificat
Page 67 and 68: MZ-3AVehicle Class: Conventional Ai
Page 69 and 70: PelicanTable 33: Pelican Program Ov
Page 71 and 72: Figure 53: Illustration Showing Lig
Page 73 and 74: Table 36: Skybus Technical Specific
Page 75 and 76: APPENDICESAppendix A- BalloonsIntro
Page 77 and 78: could be separated from the balloon
Page 79 and 80: Appendix B - Glossary of TermsAAero
Page 81 and 82: ATECAVAWSSBBAAVBCTBLOSCC2C3IC4ISRC5
Page 83 and 84: IFFIPTISRITSJJCTDJIEDDOJMUAJROCJUON
Page 85: SIGINTSINCGARSSIPRNetSMDBLSMDCSRVSu
Page 89 and 90: 43. “Lockheed Martin ISIS”. HIS
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