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Full-Scale Transport controlled Impact DemonstrationThe controlled impact demonstration (CID) test of a transport aircraft took place on December 1, 1984, crashing at a prepared site on Rogers Dry Lakebed, Edwards Air Force Base, California. The demonstration was a setback for the antimisting kerosene (AMK) researchers. The impact conditions, considerably different from the planned scenario, exposed large quantities of degraded AMK and hydraulic fluid and caused unexpectedly hot ignition sources, bulk loss of fuel from the right wing, airflow patterns over the wings and fuselage that were untested on AMK, and fuel intrusion into the lower fuselage. The test was much more severe than planned and is generally considered to be unrepresentative of the type of survivable crash that would benefit from AMK. Ninety-seven percent of the sensors on the fuselage and wing structure, seats, dummies, restraint systems, galley, and bins were active at impact. A wealth of sensor data was collected from this once-in-a-lifetime research test. The flight data recorder experiments on board were also generally successful.
Document ID
19860012462
Acquisition Source
Legacy CDMS
Document Type
Conference Proceedings
Authors
Hayduk, R. J.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 5, 2013
Publication Date
January 1, 1986
Subject Category
Structural Mechanics
Report/Patent Number
NAS 1.55:2395
NASA-CP-2395
L-16048
Report Number: NAS 1.55:2395
Report Number: NASA-CP-2395
Report Number: L-16048
Accession Number
86N21933
Funding Number(s)
PROJECT: RTOP 505-33-53-05
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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