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NASA NTRS · 19660038593

Minimum two-impulse transfer between coplanar circular orbits.

Abstract

First-order perturbation solution to problem of minimum-fuel orbit transfer in form of equal slope guidance constraint

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BibTeXRIS

Koenke, E. J.. 1966-01-01. Minimum two-impulse transfer between coplanar circular orbits.. https://ntrs.nasa.gov/citations/19660038593

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