Publication Date:
2019-07-13
Description:
Secondary or abort mission maximized subject to primary mission constraints by variational treatment of optimal branched trajectories
Keywords:
SPACE VEHICLES
Type:
AAS PAPER 68-138
,
AMERICAN ASTRONAUTICAL SOCIETY AND AMERICAN INST. OF AERONAUTICS AND ASTRONAUTICS, ASTRODYNAMICS SPECIALIST CONFERENCE; Sep 03, 1968 - Sep 05, 1968; JACKSON, WYO.|; VUE TECHNIQUE CECLES
Format:
text
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