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
Sedrick, A. V.
Publications and source records attributed to Sedrick, A. V..
Cathode studies of a radiation cooled MPD arc thruster
Cathode geometry effect on performance of radiation cooled MPD arc thrustor in continuous mode
Esker, D. W.↗