The simulation of high pressure hydrogen/oxygen rocket engines
7th Aerodynamic Testing Conference ; 1972 ; Palo Alto , CA , U.S.A.
1972-01-01
Aufsatz (Konferenz)
Elektronische Ressource
Englisch
Mathematical simulation of hydrogen–oxygen combustion in rocket engines using LOGOS code
Online Contents | 2014
|Design Criteria for High-Pressure Rocket Engines
NTIS | 1967
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