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Aerodynamic Heating Tests Of Missile Stabilizers In A Free Jet At Mach Number 2Aerodynamic heating tests of missile stabilizers in free jet at supersonic speeds
Document ID
19630004025
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Vosteen, L. F. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 2, 2013
Publication Date
September 1, 1960
Subject Category
Auxiliary Systems
Report/Patent Number
NASA-TM-X-299
Report Number: NASA-TM-X-299
Accession Number
63N13901
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
SUPERSONIC SPEED
AERODYNAMIC HEATING
FREE JET
MISSILE STABILIZATION

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