Preliminary identification and evaluation of promising LO2/Hydrocarbon rocket engine cycles were used to produce a consistent and reliable data base for vehicle optimization and design studies. cycles G and C were chosen for design analysis. Preliminary design analysis of the heat transfer subsystem was performed to establish major technology requirements.
Advanced Oxygen-Hydrocarbon Rocket Engine Study
1980
25 pages
Report
Keine Angabe
Englisch
Rocket Engines & Motors , Rocket Propellants , Cryogenic rocket propellants , Hydrocarbon fuels , Liquid propellant rocket engines , Rocket engine design , Booster rocket engines , Data bases , Graphs (Charts) , Liquid oxygen , Orbit transfer vehicles , Propulsive efficiency , Space shuttle boosters , Systems engineering , Tables (Data)
Advanced oxygen-hydrocarbon rocket engine study
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