A propulsion system analysis of the dual fuel, dual throat engine for launch vehicle applications was conducted. Basic dual throat engine characterization data were obtained to allow vehicle optimization studies to be conducted. A preliminary baseline engine system was defined.


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    Heat Flux In A Dual-Throat Rocket Engine

    Ewen, R. L. / Obrien, C. J. | NTRS | 1989



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    Bellandi, E. / Slippey, A. / American Institute of Aeronautics and Asronautics | British Library Conference Proceedings | 2009