Spacecraft rendezvous trajectory between two elliptical orbits is determined by optimization of the two impulse orbital transfer
OPTIMUM TWO-IMPULSE ORBITAL TRANSFER AND RENDEZVOUS BETWEEN INCLINED ELLIPTICAL ORBITS
21.08.1963
Preprint
Keine Angabe
Englisch
Optimum two-impulse orbital transfer and rendezvous between inclined elliptical orbits
Engineering Index Backfile | 1963
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