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Performance of Apollo block 2 thrust vector control using the PGNCS /Primary Guidance Navigation and Control System/ - Project ApolloComputerized performance evaluation of Apollo thrust vector digital autopilot control system
Document ID
19700025290
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Smith, E. E., Jr. (NASA Lyndon B. Johnson Space Center Houston, TX, United States)
Date Acquired
September 2, 2013
Publication Date
April 8, 1969
Subject Category
Navigation
Report/Patent Number
MSC-69-EG-18
NASA-TM-X-64369
Report Number: MSC-69-EG-18
Report Number: NASA-TM-X-64369
Accession Number
70N34606
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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