It is shown that the optimum transfer from one orbit to another can be accomplished only when the two orbits are coplanar. For two coplanar intersecting orbits the procedure of finding the optimum orientation of one orbit relative to the other is discussed. Numerical results are tabulated for various orbital geometries. (Author)
Optimum Orbit Transfer by Impulse
1959
50 pages
Report
No indication
English
Optimum two-impulse orbital transfer program
NTRS | 1965
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