Minimum impulse transfer between circular orbit and hyperbolic trajectory velocity vector, assuming fixed transfer times
Optimal nonplanar escape from circular orbits
AMERICAN ASTRONAUTICAL SOCIETY AND AMERICAN INST. OF AERONAUTICS AND ASTRONAUTICS, ASTRODYNAMICS CONFERENCE ; 1970 ; SANTA BARBARA, CA
1970-08-01
Conference paper
No indication
English
Optimal nonplanar escape from circular orbits
AIAA | 1970
|Optimal Nonplanar Escape from Circular Orbits
AIAA | 1971
|