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- W2329776338 abstract "The linear rocket engine is shown to be a viable candidate propulsion system for post-Space Shuttle single-stage-to-orbit systems. The linear engine system has been developed and fired demonstrating high performance and long life with firing durations exceeding 500 seconds. The application of the split or dual combustor to the linear engine permits the uses of two different propellant combinations in a single engine system. The split combustor possesses the advantages of the two position extendible bell nozzle in a fixed nozzle configuration. Engine power cycles and applications to typical vehicles are discussed." @default.
- W2329776338 created "2016-06-24" @default.
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- W2329776338 date "1975-08-16" @default.
- W2329776338 modified "2023-09-27" @default.
- W2329776338 title "Linear rocket engines for advanced space transportation systems" @default.
- W2329776338 cites W1969894548 @default.
- W2329776338 doi "https://doi.org/10.2514/6.1975-1251" @default.
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