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64. Morris, Jeff. “Air Force Backs Away from Near Space Maneuvering Vehicle”. AviationWeek. March 18 2005.http://www.aviationweek.com/aw/generic/story_generic.jsp?channel=aerospacedaily&id=news/NSMV03185. xml&headline=Air%20Force%20Backs%20Away%20From%20Near-Space%20Maneuvering%20Vehicle65. Image obtained from The Nav Log available at http://www.navlog.org/nsmv.html66. Appropriations Request Form, Oregon House Delegation. Fiscal Year 2010. Project Title:High Altitude Shuttle System (HASS).67. Website—High Altitude Shuttle System, Near Space Corporation. NASA FlightOpportunities Program. Available athttps://flightopportunities.nasa.gov/platforms/balloon/high-altitude-shuttle-system.68. Information provided by interview with representatives from GNSS (Near Space SystemsInc.) and the Star Light development team.69. “Providing National Security on Far Fewer Dollars”, GNSS press release. Available athttp://www.globalnea-rspace.com/press_release_SPSA.shtml.D-4
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SUMMARY REPORT OF DoD FUNDED LIGHTE
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TABLE OF CONTENTSEXECUTIVE SUMMARY
Page 5 and 6:
Figure 11: Computer Rendering of Al
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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
Page 33 and 34:
Table 7: JLENS Technical Specificat
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Persistent Ground Surveillance Syst
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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 and 86: SIGINTSINCGARSSIPRNetSMDBLSMDCSRVSu
Page 87 and 88: Appendix D - References1. The Senat
Page 89: 43. “Lockheed Martin ISIS”. HIS
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