Add to ORKGAmmonia fueled resistojet thrustor system for three-axis attitude control and two-direction station-keeping of stable platform type satellit
Ignition characteristics and delivered performance of gaseous hydrogen-oxygen reaction control thrus...
Solid propellant rocket engine environmental and static testing for use as retrograde thrustor in At...
Electric switchgear for space nuclear power - vacuum interrupter switch and actuato
Design, development, fabrication, evaluation, and delivery of electrothermal, three axis, spacecraft...
A flight-qualified electrothermal thruster demonstrated its adaptability to a variety of propellants...
Alternating current circuit breakers and direct current engine contactors for space nuclear electric...
Radiation-cooled and water-cooled magnetoplasmadynamic thrustors tested in 10 to kW power range with...
Venting system for use with cryogenic propellants to control tank pressure during zero-gravity coas
Alternating current circuit breaker and direct current engine contactors for space - vacuum interru...
Engine control system design for 2 to 15 kWe Brayton power system for space station
Design, fabrication, life testing, and supporting research of cesium contact ion rocket engin
Electrically heated and radioisotope heated thrusters for satellite attitude control and stationkeep...
Heat balances of combined astrionic equipment and thermal conditioning subsystem of environmental co...
Test data taken with nitrogen, hydrogen, and ammonia propellants are presented over a wide range of ...
Experimental tube design, vacuum system, technique for studying electron and ion emission from cesia...
Ignition characteristics and delivered performance of gaseous hydrogen-oxygen reaction control thrus...
Solid propellant rocket engine environmental and static testing for use as retrograde thrustor in At...
Electric switchgear for space nuclear power - vacuum interrupter switch and actuato
Design, development, fabrication, evaluation, and delivery of electrothermal, three axis, spacecraft...
A flight-qualified electrothermal thruster demonstrated its adaptability to a variety of propellants...
Alternating current circuit breakers and direct current engine contactors for space nuclear electric...
Radiation-cooled and water-cooled magnetoplasmadynamic thrustors tested in 10 to kW power range with...
Venting system for use with cryogenic propellants to control tank pressure during zero-gravity coas
Alternating current circuit breaker and direct current engine contactors for space - vacuum interru...
Engine control system design for 2 to 15 kWe Brayton power system for space station
Design, fabrication, life testing, and supporting research of cesium contact ion rocket engin
Electrically heated and radioisotope heated thrusters for satellite attitude control and stationkeep...
Heat balances of combined astrionic equipment and thermal conditioning subsystem of environmental co...
Test data taken with nitrogen, hydrogen, and ammonia propellants are presented over a wide range of ...
Experimental tube design, vacuum system, technique for studying electron and ion emission from cesia...
Ignition characteristics and delivered performance of gaseous hydrogen-oxygen reaction control thrus...
Solid propellant rocket engine environmental and static testing for use as retrograde thrustor in At...
Electric switchgear for space nuclear power - vacuum interrupter switch and actuato