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BI-ELLIPTIC TRANSFER WITH PLANE CHANGE
[report]
1965
unpublished
This technical documentary report has been reviewed and is approved for publication and dissemination. The conclusions and findings contained herein do not necessarily represent an official Air Force position. William E. O'Brien Lt, USAF Project Officer •in-ABSTRACT By the calculations presented, the minimum total velocity increment required for bi-elliptic transfer between non-coplanar circular orbits is obtained. The maneuver considered is the following: A vehicle in circular orb't at
doi:10.21236/ad0476156
fatcat:4fe3reqk5fcn3mlmxfnw3l2c2i