Cathode studies of a radiation cooled MPD arc thruster
Cathode insulator modifications of radiation cooled MPD arc thrustor tested in power range of 9.8 to 46.4 kW using ammonia as principal propellant
Esker, D. W.↗
Engineering topics
Publications and source records attributed to Kroutil, J. C..
Cathode insulator modifications of radiation cooled MPD arc thrustor tested in power range of 9.8 to 46.4 kW using ammonia as principal propellant
Cathode geometry effect on performance of radiation cooled MPD arc thrustor in continuous mode
Radiation cooled MPD arc thrustor design and performance, noting specific impulse relation to arc spoke rotation frequencies
Local mass flux and local impact pressure measurement in arc jet exhaust flow fields
Energy transfer mechanisms in radiation, water, and regeneratively cooled, and MPD arc jet propulsion devices