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- W2325206823 abstract "This paper describes the conceptual design of the RS-2100 Full-Flow Stage Combustion rocket engine. This engine was developed for application to SSTO RLVs. The advantages of the Full-Flow cycle are; low turbine temperatures, simplification of the High Pressure Oxidizer Turbopump, safe LOX heat exchanger and robust gas spin start." @default.
- W2325206823 created "2016-06-24" @default.
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- W2325206823 date "1997-07-06" @default.
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- W2325206823 title "Advantages of a full-flow staged combustion cycle engine system" @default.
- W2325206823 doi "https://doi.org/10.2514/6.1997-3318" @default.
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