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Oxygen rich gas generator design and performance analysisThe present oxygen-rich combustion research investigates oxygen gas generator concepts. The theoretical and modeling aspects of a selected concept are presented, together with a refined concept resulting from the findings of the study. This investigation examined a counter-flow gas generator design for O2/H2 mass ratios of 100-200, featuring a near-stoichiometric combustion zone followed by downstream mixing. The critical technologies required to develop a performance model are analyzed and include the following: (1) oxygen flow boiling; (2) two-phase oxygen flow heat transfer; (3) film-cooling in the combustion zone; (4) oxygen-rich combustion with hydrogen; and (5) mixing and dilution.
Document ID
19930065978
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Gloyer, P. W.
(NASA Headquarters Washington, DC United States)
Knuth, W. H.
(NASA Headquarters Washington, DC United States)
Crawford, R. A.
(Tennessee Univ. Tullahoma, United States)
Date Acquired
August 16, 2013
Publication Date
June 1, 1993
Subject Category
Spacecraft Propulsion And Power
Report/Patent Number
AIAA PAPER 93-2159
Meeting Information
Meeting: AIAA, SAE, ASME, and ASEE, Joint Propulsion Conference and Exhibit
Location: Monterey, CA
Country: United States
Start Date: June 28, 1993
End Date: June 30, 1993
Sponsors: ASEE, ASME, AIAA, SAE
Accession Number
93A49975
Funding Number(s)
CONTRACT_GRANT: NAGW-1195
Distribution Limits
Public
Copyright
Other

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