NASA NTRS · 19630028696
ORBITAL RENDEZVOUS CONSIDERATIONS FOR A MARS MISSION
Abstract
Orbital rendezvous considerations for mars mission requiring tangential approach to, and departure from, orbit to achieve maximum propulsive efficiency
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Bird, J. D., Thomas, D. F.. 1963-01-01. ORBITAL RENDEZVOUS CONSIDERATIONS FOR A MARS MISSION. https://ntrs.nasa.gov/citations/19630028696
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