Experimental Rocket Performance of APOLLO Storable Propellants in Engines with Large Area Ratio Nozzles
1966
45 pages
Report
Keine Angabe
Englisch
Rocket Propellants , Apollo project , Hydrazine , Nitrogen oxide , Rocket nozzle , Storable propellant , Chamber , Combustion , Dimethyl , Module , Nitrogen , Nozzle , Oxide , Propellant , Rocket , Rocket engine , Service , Storage , Supersonic , Thrust , Unsymmetrical