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HEATING AND IMPACT TESTS ON INSULATED AND UNINSULATED BALLISTICMISSILE FUSE MECHANISMS SUBJECTED TO SIMULATED REENTRY AERODYNAMIC HEATINGHeat & impact test on insulated & uninsulated fuse mechanism of ballistic missile in reentry aerodynamic heating
Document ID
19630004882
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Memorandum (MEMO)
Authors
Nix, W. L. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 2, 2013
Publication Date
January 1, 1959
Subject Category
Aircraft
Report/Patent Number
NASA-MEMO-12-5-58L
Report Number: NASA-MEMO-12-5-58L
Accession Number
63N14758
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
BALLISTIC MISSILE
IMPACT TEST
AERODYNAMIC HEATING
INSULATED STRUCTURE
HEAT TEST
FUSE
REENTRY
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