Refractory Thrust Chambers for Spacecraft Engines Final Report
1965
156 pages
Report
Keine Angabe
Englisch
Rocket Engines & Motors , Liquid propellant rocket engine , Pyrolytic graphite , Rocket nozzle , Structural reliability , Alloy , Chamber , Crystal , Graphite , Heat , Liquid , Nozzle , Pressure , Propellant , Pyrolysis , Reliability , Rocket , Rocket engine , Rupture , Structural , Structure , Thin , Thrust , Thrust chamber , Treatment , Tube , Wall
Coatings for advanced thrust chambers Final report
NTRS | 1968
|Advanced thrust chambers for miniaturized engines
AIAA | 1992
|