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Utilization and characteristic velocity saving with a small throttleable region about 92.5 per cent thrust for LM powered descentUtilizing small throttling capability about high thrust region of 92.5 % for lunar module powered descent
Document ID
19700026566
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Mc Swain, G. G. (NASA Lyndon B. Johnson Space Center Houston, TX, United States)
Moore, T. E. (NASA Lyndon B. Johnson Space Center Houston, TX, United States)
Date Acquired
September 2, 2013
Publication Date
November 22, 1967
Subject Category
Navigation
Report/Patent Number
NASA-TM-X-65077
MSC-IN-67-EG-34
Report Number: NASA-TM-X-65077
Report Number: MSC-IN-67-EG-34
Accession Number
70N35882
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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