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DESIGN CRITERIA FOR ZERO-LEAKAGE CONNECTORS FOR LAUNCH VEHICLES, VOLUME 6 - ENVIRONMENTAL EFFECTSPressure pulses, shock and vibratory loading on launch vehicle connectors - heat environment, vacuum and radiation effects on connector gaskets
Document ID
19630008446
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Levy, S. (General Electric Co. Schenectady, NY, United States)
Date Acquired
September 2, 2013
Publication Date
March 15, 1963
Subject Category
Materials, Metallic
Report/Patent Number
NASA-CR-50562
Report Number: NASA-CR-50562
Accession Number
63N18323
Funding Number(s)
CONTRACT_GRANT: NAS8-4012
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
LAUNCH VEHICLE
SHOCK LOAD
RADIATION EFFECT
VACUUM
PRESSURE PULSE
VIBRATORY LOADING
THERMAL ENVIRONMENT
GASKET

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