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NASA NTRS · 19930065978

Oxygen rich gas generator design and performance analysis

Abstract

The 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.

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BibTeXRIS

Gloyer, P. W., Knuth, W. H., Crawford, R. A.. 1993-06-01. Oxygen rich gas generator design and performance analysis. https://ntrs.nasa.gov/citations/19930065978

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