Experimental and analytical investigation of the dynamic response of a supersonic mixed-compression inlet
Experimental and analytical investigation of dynamic response of supersonic mixed-compression inlet
Wasserbauer, J. F.↗
Engineering topics
Wasserbauer, J. F.
Publications and source records attributed to Wasserbauer, J. F..
Experimental mercury bombardment thruster at submillipound thrust.
Ion thrustor, including mercury feed system and shielded neutralizer, designed and tested for spacecraft station keeping and attitude control
ATTITUDE CONTROL↗
A 5-centimeter-diameter electron-bombardment thrustor with permanent magnets
Permanent magnet electron bombardment ion thrustor for station keeping and attitude control of synchronous satellite
ELECTRON BOMBARDMENT↗
A mercury electron-bombardment ion thrustor suitable for spacecraft station keeping and attitude control.
Ion thrustor, including mercury feed system and shielded neutralizer, designed and tested for spacecraft station keeping and attitude control
SPACECRAFT CONTROL↗
A mercury electron-bombardment ion thrustor suitable for spacecraft station keeping and altitude control
Mercury electron bombardment ion thrustor with radial flow propellant distributor for spacecraft attitude control
MERCURY /METAL/↗
EXPERIMENTAL PERFORMANCE OF A HIGH-CURRENT-DENSITY CYLINDRICAL CONCAVE POROUS TUNGSTEN EMITTER FOR ION THRUSTORS
Performance of a high current density cylindrical concave porous tungsten emitter for cesium propellant ion thrustors
CESIUM ENGINE↗
Performance of a 28-inch ramjet utilizing gaseous hydrogen at a mach number of 3.6, angles of attack up to 12 deg, and pressure altitudes up to 110,000 feet
Combustion efficiency of gaseous hydrogen fuel for ramjets at very high altitudes and high distortion
HYDROGEN FUEL↗