Optimal finite-thrust transfer between planet approach and departure asymptotes with specified intermediate orbit
Optimal finite-thrust transfer between planet approach and departure asymptotes with specified intermediate orbit
1968-04-01
Miscellaneous
No indication
English
OPTIMUM TRANSFERS BETWEEN HYPERBOLIC ASYMPTOTES
AIAA | 1963
|Optimal, Low-Thrust, EarthMoon Orbit Transfer
AIAA | 1998
|