Multimission solar electric spacecraft propulsion module design for Asteroid Belt, Jupiter and out-of-ecliptic missions, including thrustor failure and power conditioning requirements
Propulsion module design for a multimission solar electric spacecraft
AMERICAN INST. OF AERONAUTICS AND ASTRONAUTICS, ELECTRIC PROPULSION CONFERENCE, 8TH ; 1970 ; STANFORD, CA
1970-08-01
Conference paper
No indication
English