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Apollo 14 flight support and system performanceThe Apollo 13 incident and subsequent oxygen tank redesign for Apollo 14 placed unique requirements on the flight support activity. A major part of this activity was the integration of the various analytical efforts into a single team function. Additionally, the first flight of the redesigned system without an orbital test required an extensive analytical base. The support team philosophy, objectives, and organization are presented. Various analytical tools that were used during the flight are discussed. Investigations made during the postflight period are considered and their impact upon subsequent flights shown.
Document ID
19720016152
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Rice, R. R.
(NASA Lyndon B. Johnson Space Center Houston, TX, United States)
Date Acquired
August 6, 2013
Publication Date
May 1, 1971
Publication Information
Publication: MSC Cryog. Symp. Papers p488-509 (SEE N72-23785 14-27)
Subject Category
Space Vehicles
Accession Number
72N23802
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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