Design of Injectors and Ablative Thrust Chambers for a Flox-Propane Rocket Engine with a 1.2-Inch Throat Diameter
1969
38 pages
Report
Keine Angabe
Englisch
Improved Throat Inserts for Ablative Thrust Chambers
NTIS | 1967
|Improved throat inserts for ablative thrust chambers
NTRS | 1967
|