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- W760333883 abstract "An evaluation of reusable thrust chambers for the space shuttle orbit maneuvering engine was conducted. Tests were conducted using subscale injector hot-fire procedures for the injector configurations designed for a regenerative cooled engine. The effect of operating conditions and fuel temperature on combustion chamber performance was determined. Specific objectives of the evaluation were to examine the optimum like-doublet element geometry for operation at conditions consistent with a fuel regeneratively cooled engine (hot fuel, 200 to 250 F) and the sensitivity of the triplet injector element to hot fuels." @default.
- W760333883 created "2016-06-24" @default.
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- W760333883 date "1974-01-30" @default.
- W760333883 modified "2023-09-27" @default.
- W760333883 title "Space shuttle orbit maneuvering engine, reusable thrust chamber program. Task 6: Data dump hot fuel element investigation" @default.
- W760333883 hasPublicationYear "1974" @default.
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