The status of monopropellant hydrazine technology
Hydrazine properties, catalysts for hydrazine decomposition, catalytic reaction chambers, and monopropellant hydrazine thrustor
Evans, D. D.↗
Engineering topics
Evans, D. D.
Publications and source records attributed to Evans, D. D..
The effect of injector-element scale on the mixing and combustion of nitrogen tetroxide-hydrazine propellants
Injector-element physical size effect on mixing and combustion of nitrogen tetroxide-hydrazine propellants
Evans, D. D.↗
Ignition means for monopropellant Patent
Catalyst bed ignition system for hydrazine propellants
Evans, D. D.↗
Development of the Ranger Block III SPACECRAFT propulsion system
Design, development, and flight operation of midcourse propulsion system used on Ranger Block III spacecraft
PROPULSION SYSTEM↗
On the evolution of advanced propulsion systems for spacecraft
Use of earth-storable propellants in unmanned spacecraft propulsion systems for flights to near planets and moon
EARTH↗
Advanced liquid propulsion systems
Advanced liquid propellants for spacecraft propulsion - nitrogen tetroxide and hydrazine
PROPULSION↗
Designing for compatibility in high-performance lp engines.
Quantitative design criteria for priori injector designs yielding combustion process compatible with thrust chamber-nozzle materials
PROPELLANT COMBUSTION↗
Advanced propulsion systems for unmanned spacecraft.
Advanced propulsion systems for unmanned spacecraft making simple pressure-fed systems, using storable propellants, thrust chambers and flexible propellant barriers
UNMANNED SPACECRAFT↗
THE DEVELOPMENT OF A HEATED-HYBRID GENERATED GAS PRESSURIZATION SYSTEM FOR PROPELLANT TANKS
Heated-hybrid generated gas pressurization system for liquid propellant transfer in rocket vehicles
GAS PRESSURE↗