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Performance analysis of the ascent propulsion system of the Apollo spacecraftActivities involved in the performance analysis of the Apollo lunar module ascent propulsion system are discussed. A description of the ascent propulsion system, including hardware, instrumentation, and system characteristics, is included. The methods used to predict the inflight performance and to establish performance uncertainties of the ascent propulsion system are discussed. The techniques of processing the telemetered flight data and performing postflight performance reconstruction to determine actual inflight performance are discussed. Problems that have been encountered and results from the analysis of the ascent propulsion system performance during the Apollo 9, 10, and 11 missions are presented.
Document ID
19740005391
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Technical Note (TN)
Authors
Hooper, J. C., III
(NASA Lyndon B. Johnson Space Center Houston, TX, United States)
Date Acquired
September 3, 2013
Publication Date
December 1, 1973
Subject Category
Propulsion Systems
Report/Patent Number
JSC-S-354
NASA-TN-D-7400
Report Number: JSC-S-354
Report Number: NASA-TN-D-7400
Accession Number
74N13504
Funding Number(s)
PROJECT: RTOP 914-50-60-07-72
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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