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Qualification evaluation of the pitch control motor for the launch escape system of the Apollo spacecraft programEnvironmental testing and static firing of pitch control motor for Apollo spacecraft launch escape system
Document ID
19670024883
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Technical Note (TN)
Authors
Cota, P. E., Jr.
Lee, B. J.
Date Acquired
September 2, 2013
Publication Date
August 1, 1967
Subject Category
Space Vehicles
Report/Patent Number
NASA-TN-D-4068
Report Number: NASA-TN-D-4068
Accession Number
67N34212
Funding Number(s)
CONTRACT_GRANT: 914-11-10-00-72
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
ESCAPE ROCKET
PITCH CONTROLLER
STATIC FIRING
APOLLO SPACECRAFT
ENVIRONMENTAL TESTING

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