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NASA NTRS · 19670048807

Optimum deorbit positioning for minimum impulse reentry.

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Abstract

Optimum deorbit positioning on planetocentric elliptic orbit for single impulse reentry treated by two coupled quartic polynomials

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REENTRY PHYSICS IMPULSE ORBITAL TRANSFER ELLIPTICAL ORBIT TRAJECTORY OPTIMIZATION

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Stern, G. S.. 1967-01-01. Optimum deorbit positioning for minimum impulse reentry.. https://ntrs.nasa.gov/citations/19670048807

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