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Apollo experience report: Abort planningDefinition of a practical return-to-earth abort capability was required for each phase of an Apollo mission. A description of the basic development of the complex Apollo abort plan is presented. The process by which the return-to-earth abort plan was developed and the constraining factors that must be included in any abort procedure are also discussed. Special emphasis is given to the description of crew warning and escape methods for each mission phase.
Document ID
19720017278
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Technical Note (TN)
Authors
Hyle, C. T.
(NASA Lyndon B. Johnson Space Center Houston, TX, United States)
Foggatt, C. E.
(NASA Lyndon B. Johnson Space Center Houston, TX, United States)
Weber, B. D.
(NASA Lyndon B. Johnson Space Center Houston, TX, United States)
Date Acquired
September 2, 2013
Publication Date
June 1, 1972
Subject Category
Space Vehicles
Report/Patent Number
NASA-TN-D-6847
MSC-S-307
Accession Number
72N24928
Funding Number(s)
PROJECT: RTOP 924-22-20-00-72
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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