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NASA NTRS · 19670013939

Optimum two-impulse orbital transfer program

Hoy, R. C.·Mc Cue, G. A.

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Abstract

Computer method to determine optimum two-impulse orbital transfers between inclined elliptical orbits

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COMPUTER METHOD ELLIPTICAL ORBIT ORBITAL TRANSFER

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Hoy, R. C., Mc Cue, G. A.. 1965-08-01. Optimum two-impulse orbital transfer program. https://ntrs.nasa.gov/citations/19670013939

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