None given. From statement of problem:The broad nature of this work has been to extend our understanding of the nature of the conventional or classical hybrid rocket combustion process (fuel decomposition, heat and mass transfer, and chemical reaction), and the critical engineering parameters that define this process.
Characterization of Hybrid Rocket Internal Heat Flux and HTPB Fuel Pyrolysis
27.06.1994
Sonstige
Keine Angabe
Englisch
combustion , hydroxyl , plybutadiene , terminated , pyrolysis , process , fuels , law , HTPB , rocket
Characterization of Hybrid Rocket Internal Heat Flux and HTPB Fuel Pyrolysis
British Library Conference Proceedings | 1994
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