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Remote control of an impact demonstration vehicleUplink and downlink telemetry systems were installed in a Boeing 720 aircraft that was remotely flown from Rogers Dry Lake at Edwards Air Force Base and impacted into a designated crash site on the lake bed. The controlled impact demonstration (CID) program was a joint venture by the National Aeronautics and Space Administration (NASA) and the Federal Aviation Administration (FAA) to test passenger survivability using antimisting kerosene (AMK) to inhibit postcrash fires, improve passenger seats and restraints, and improve fire-retardent materials. The uplink telemetry system was used to remotely control the aircraft and activate onboard systems from takeoff until after impact. Aircraft systems for remote control, aircraft structural response, passenger seat and restraint systems, and anthropomorphic dummy responses were recorded and displayed by the downlink stems. The instrumentation uplink and downlink systems are described.
Document ID
19850015486
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Harney, P. F.
(NASA Ames Research Center Moffett Field, CA, United States)
Craft, J. B., Jr.
(NASA Ames Research Center Moffett Field, CA, United States)
Johnson, R. G.
(NASA Ames Research Center Moffett Field, CA, United States)
Date Acquired
September 5, 2013
Publication Date
April 1, 1985
Subject Category
Aircraft Instrumentation
Report/Patent Number
H-1282
PAPER-542
NASA-TM-85925
NAS 1.15:85925
Report Number: H-1282
Report Number: PAPER-542
Report Number: NASA-TM-85925
Report Number: NAS 1.15:85925
Meeting Information
Meeting: Intern. Instrumentation Symp. of the Instrument Soc. of Am.
Location: San Diego, CA
Country: United States
Start Date: May 6, 1985
End Date: May 9, 1985
Accession Number
85N23797
Funding Number(s)
PROJECT: RTOP 505-45-11
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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