V Earth-to-Moon TrajectoriesV Earth-to-Moon trajectories has been initiated. Numerical integration of the equations of motion from the circular restricted three-body problem has resulted in the computation of a trajectory that saves more that 100 m/s over a Hohmann transfer, although the flight time is almost ten months.Document ID
20060037953
Acquisition Source
Jet Propulsion Laboratory
Document Type
Preprint (Draft being sent to journal)
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Authors
Date Acquired
August 23, 2013
Publication Date
August 1, 1994
Subject Category
Distribution Limits
Public
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Other
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