NASA NTRS · 19650026352
Study of direct-return rendezvous trajectories using constant-thrust engines and rendezvous or maneuvering thrusters
Abstract
Effect of using two separate engines in lunar lander for direct-return rendezvous with vehicle
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Fletcher, H. S., Williams, J. L.. 1965-10-01. Study of direct-return rendezvous trajectories using constant-thrust engines and rendezvous or maneuvering thrusters. https://ntrs.nasa.gov/citations/19650026352
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