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New considerations for pogo prevention on space shuttleRecommendations for improving the methodology of pogo suppression for the space shuttle include: Consideration of inter-pump location for accumulator or active device, inclusion of tank outflow effects in dynamic structural analysis, the use of simplified transfer functions in systems studies, three phase dynamic testing program for turbopump with development of dynamic flowmeters, and the use of a linearized mathematical model for engine physics studies.
Document ID
19720023220
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Rubin, S.
(Aerospace Corp. El Segundo, CA, United States)
Date Acquired
August 6, 2013
Publication Date
July 1, 1972
Publication Information
Publication: NASA, Washington NASA Space Shuttle Technol. Conf.
Subject Category
Space Vehicles
Accession Number
72N30870
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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