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.
Dual-Fuel, Dual-Throat Engine Preliminary Analysis
1979
235 pages
Report
No indication
English
Rocket Engines & Motors , Space Launch Vehicles & Support Equipment , Engine tests , Propulsion system configurations , Propulsion system performance , Rocket engine design , Rocket engines , Thrust chambers , Engine parts , Launch vehicles , Liquid rocket propellants , Rocket nozzles , Rocket thrust , Single stage to orbit vehicles , Structural analysis , Thrust chamber pressure , Thrust-weight ratio
Dual-fuel, dual-throat engine preliminary analysis
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