Effect of oxidizer particle size on solid- propellant combustion stability
Oxidizer particle size effect on solid propellant combustion stability
OXIDIZER↗
Engineering topics
Morrell, G.
Publications and source records attributed to Morrell, G..
RATE OF LIQUID JET BREAKUP BY A TRANSVERSE SHOCK WAVE
Breakup of water jet by transverse shock wave
SHOCK WAVE↗
Method for continuous variation of propellant flow and thrust in propulsive devices Patent
Continuous variation of propellant flow and thrust by application of liquid foam flow theory to injection orifice
Morrell, G.↗
BREAKUP OF LIQUID JETS BY TRANSVERSE SHOCKS
Multiple shock waves impinging on a single liquid jet and on two parallel jets in a direction perpendicular to their flow axes
SHOCK WAVE↗
LOW-TEMPERATURE CHEMICAL STARTING OF A 200-POUND-THRUST JP-4 - NITRIC ACID ROCKET ENGINE USING A THREE-FLUID PROPELLANT VALVE
Low-temperature chemical starting of combined jp-4 nitric acid propellant for low-thrust rocket engine using three-fluid propellant valve
ROCKET ENGINE↗