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The Apollo 15 deployable boom anomalyDuring the Apollo 15 mission, a boom with an attached mass spectrometer was required to retract periodically so that the instrument would not be in the field of view of other experiments. The boom did not fully retract on five of 12 occasions. Data analysis indicated that the boom probably retracted to within approximately 2.54 centimeters (1 inch) of full retraction. The pertinent boom-design details, the events in the mission related to the anomaly, a discussion of the inflight and postflight investigation of the problem, a discussion of the design changes to the boom mechanism as a result of the investigation, and subsequent flight performance are presented.
Document ID
19730010141
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
White, R. D.
(NASA Lyndon B. Johnson Space Center Houston, TX, United States)
Date Acquired
August 7, 2013
Publication Date
November 1, 1972
Publication Information
Publication: the 7th Aerospace Mech. Symp.
Subject Category
Space Vehicles
Accession Number
73N18868
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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