Add to ORKGIgnition characteristics and delivered performance of gaseous hydrogen-oxygen reaction control thrus...
Techniques for rating performance of ablative materials in liquid-propellant rocket engine
Activation and initial test operations of thrust chamber facility for NASA M-1 rocket engin
Design, development, and life tests of electron bombardment cesium ion engine system, permanent magn...
Ionization studies dealing with ion source, emission contamination, and alkali desorption energies o...
Electron bombardment, mercury-fueled ion engine system - investigation, testing, and development pro...
Experimental tube design, vacuum system, technique for studying electron and ion emission from cesia...
Surface ionization studies on refractory metals and metal alloys used in long term contact ion engin...
Operational performance of electron bombardment mercury ion thruster system during life testing in s...
Computer program written in IBM 7090 Fortran II FOR analyzing space charge flow in electron or ion g...
Ammonia fueled resistojet thrustor system for three-axis attitude control and two-direction station-...
Heat transfer, altitude performance, and combustion efficiency evaluated in study of space storable ...
Deflectable dual beam, linear strip cesium contact, ion thruster system design and performance testi...
Design, development, fabrication, evaluation, and delivery of electrothermal, three axis, spacecraft...
Solid propellant rocket engine environmental and static testing for use as retrograde thrustor in At...
Ignition characteristics and delivered performance of gaseous hydrogen-oxygen reaction control thrus...
Techniques for rating performance of ablative materials in liquid-propellant rocket engine
Activation and initial test operations of thrust chamber facility for NASA M-1 rocket engin
Design, development, and life tests of electron bombardment cesium ion engine system, permanent magn...
Ionization studies dealing with ion source, emission contamination, and alkali desorption energies o...
Electron bombardment, mercury-fueled ion engine system - investigation, testing, and development pro...
Experimental tube design, vacuum system, technique for studying electron and ion emission from cesia...
Surface ionization studies on refractory metals and metal alloys used in long term contact ion engin...
Operational performance of electron bombardment mercury ion thruster system during life testing in s...
Computer program written in IBM 7090 Fortran II FOR analyzing space charge flow in electron or ion g...
Ammonia fueled resistojet thrustor system for three-axis attitude control and two-direction station-...
Heat transfer, altitude performance, and combustion efficiency evaluated in study of space storable ...
Deflectable dual beam, linear strip cesium contact, ion thruster system design and performance testi...
Design, development, fabrication, evaluation, and delivery of electrothermal, three axis, spacecraft...
Solid propellant rocket engine environmental and static testing for use as retrograde thrustor in At...
Ignition characteristics and delivered performance of gaseous hydrogen-oxygen reaction control thrus...
Techniques for rating performance of ablative materials in liquid-propellant rocket engine
Activation and initial test operations of thrust chamber facility for NASA M-1 rocket engin