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Investigation and modeling of space shuttle main engine shutdown transient chuggingThe space shuttle main engines experience a low frequency pressure pulsation in both the fuel and oxidizer preburners during the shutdown transient. This pressure pulsation, called chugging, has been linked to undesirable bearing loads and possible damage to the spark ignitor supply piping for the fuel preburner. The problem is briefly described and a model is proposed that includes: (1) a transient stirred tank reactor model for the combustion chamber, (2) a resistance capacitance model for the supply piping and (3) purge gas/liquid oxygen interface tracking.
Document ID
19860015053
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
George, P. E., II
(Tennessee Univ. Knoxville, TN, United States)
Date Acquired
August 12, 2013
Publication Date
January 1, 1986
Publication Information
Publication: NASA. Marshall Space Flight Center Research Reports: 1985 NASA(ASEE Summer Faculty Fellowship Program
Subject Category
Spacecraft Propulsion And Power
Accession Number
86N24524
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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