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
11.08.1980
Report
Keine Angabe
Englisch
Advanced oxygen-hydrocarbon rocket engine study
NTRS | 1980
|Advanced oxygen-hydrocarbon rocket engine study
NTRS | 1981
|Advanced Oxygen-Hydrocarbon Rocket Engine Study
NTIS | 1981
|Advanced Oxygen-Hydrocarbon Rocket Engine Study
NTIS | 1980
|Advanced Oxygen-Hydrocarbon Rocket Engine Study
NTIS | 1980
|