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Atomization and Mixing StudyThe primary objective was the obtainment of atomization and mixing performance data for a variety of typical liquid oxygen/hydrocarbon injector element designs. Such data are required to establish injector design criteria and to provide critical inputs to liquid rocket engine combustor performance and stability analysis, and computational codes and methods. Deficiencies and problems with the atomization test equipment were identified, and action initiated to resolve them. Test results of the gas/liquid mixing tests indicated that an assessment of test methods was required. A series of 71 liquid/liquid tests were performed.
Document ID
19860014169
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Ferrenberg, A.
(Rockwell International Corp. Canoga Park, CA, United States)
Hunt, K.
(Rockwell International Corp. Canoga Park, CA, United States)
Duesberg, J.
(Rockwell International Corp. Canoga Park, CA, United States)
Date Acquired
September 5, 2013
Publication Date
December 30, 1985
Subject Category
Spacecraft Propulsion And Power
Report/Patent Number
NAS 1.26:178751
RI/RD85-312
NASA-CR-178751
Accession Number
86N23640
Funding Number(s)
CONTRACT_GRANT: NAS8-34504
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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