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Table 25: HiSentinel 80 Technical SpecificationsLength: 194 ft.Diameter: 43 ft.Volume: 212,800 cu. ft.Max Payload: 80 lbs.Payload Type: ISRFigure 39: HiSentinel 80 Detailed Profile 39Flight ceiling: 60,000 ft.Duration: 24 hours (8 hrs. in actual test)Cruise Speed: 15–26 kts.Mass: 800 lbs.Payload Power Available: 50 WThe payload package used on the HiSentinel80 is the same as the payload used on theSMDC’s other HAA program (HALE-D),which consists of an ITT hi-resolutionelectro-optical system, a Thales MMARprototype, and an L3 CommunicationsMCDL. 37A flight test of HiSentinel 80 was conductedin November 2010 to achieve the targetaltitude, speed and duration, as well asattempt to maintain station-keepingcapability. During the test the <strong>air</strong>shipexperienced propulsion failure and landedeight hours into a planned 24-hour mission. 4HiSentinel was initiated in FY96 withfunding from Army SMDC. Fundingexpired in FY10 and no plans have beenmade to fund the project in the future.46
Table 26: Comparison of HiSentinel Aircraft Generations 12HiSentinel 20 HiSentinel 50 HiSentinel 80Year of Flight 2005 2008 2010Altitude 72,000 ft. 66,400 ft. 60,000 ft.Duration 5 hours 24 hours(3 min. in test flight)Payload 20 lbs. 50 lbs. 80 lbs.24 hours(8 hrs. in test flight)Figure 40: HiSentinel 20 (2005) 12 Figure 41: HiSentinel 50 (2008) 1247
Page 1 and 2:
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
Page 11 and 12: for unmanned aerial vehicle and cru
Page 13 and 14: Integrated Sensor Is Structure (ISI
Page 15 and 16: PREFACECongress, through the Senate
Page 17 and 18: PURPOSEThe purpose of this document
Page 19 and 20: INTRODUCTIONBackgroundModern LTA cr
Page 21 and 22: ground, large aerostats are anchore
Page 23 and 24: AirliftAirships, particularly hybri
Page 25 and 26: AEROSTAT PROGRAMSAerostats are air
Page 27 and 28: Aerostat Test Bed (ATB)Table 2: ATB
Page 29 and 30: AltusTable 4: Altus Program Overvie
Page 31 and 32: would otherwise lack organic survei
Page 33 and 34: 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: HiSentinelTable 24: HiSentinel Prog
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 and 90: 43. “Lockheed Martin ISIS”. HIS
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