Space storable thruster investigation
Design, characteristics, and test firing of radiation and film cooled 25 pound thrust graphitic thrust chamber with liquid cryogenic propellants
Engineering topics
Publications and source records attributed to Campbell, J. G..
Design, characteristics, and test firing of radiation and film cooled 25 pound thrust graphitic thrust chamber with liquid cryogenic propellants
Hermetic sealing device for ends of tubular bodies during materials testing operations
Hot firing tests with FLOX/methane propellants for evaluating pyrolytic refractory composite materials for thrust chambers
Multislot film cooled pyrolytic graphite rocket nozzle
Structural reliability tests on pyrolytic graphite and pyrolytic graphite alloys for use in liquid propellant rocket engine thrust chambers and nozzles
Cooling thrust chamber of liquid propellant rocket engine using pyrolytic graphite and hydrocarbon film
Liquid propellant rocket engine - cooling system, ablation, and heat sink
Pyrolytic graphite rocket thrust chamber
Thermal stresses in a pyrolytic graphite thrust chamber
Pyrolytic graphite thrust chamber development