Three body numerical solutions to low thrust guidance and navigation for outer planet orbiter with nuclear-electric propulsion
Some three-body numerical solutions to outer planet orbiter missions using nuclear-electric propulsion
AMERICAN ASTRONAUTICAL SOCIETY AND AMERICAN INST. OF AERONAUTICS AND ASTRONAUTICS, ASTRODYNAMICS CONFERENCE ; 1970 ; SANTA BARBARA, CA
1970-08-01
Conference paper
No indication
English