Gaseous oxygen/gaseous hydrogen auxiliary propulsion engines, considering cold flow experiments with nonreactive simulant gases
Cold-flow optimization of gaseous oxygen/gaseous hydrogen injectors for the Space Shuttle APS thruster
PROPULSION JOINT SPECIALIST CONFERENCE ; 1971 ; SALT LAKE CITY, UT, US
01.06.1971
Aufsatz (Konferenz)
Keine Angabe
Englisch
High-pressure gaseous hydrogen/gaseous oxygen thruster
AIAA | 1971
|High-pressure gaseous hydrogen/gaseous oxygen thruster
NTRS | 1971
|