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 studies of a radiation cooled MPD arc thruster
1971-05-01
Report
Keine Angabe
Englisch
Cathode studies of a radiation cooled MPD arc thruster
AIAA | 1970
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NTIS | 1971
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