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NASA NTRS ยท 19680002381

Interplanetary guidance system requirements study. Volume 2 - Computer program descriptions. Part 9 - Program description for optimum low thrust trajectories

Abstract

Computer program for optimization of low thrust interplanetary trajectories assuming constant and continuous thrust from given initial and final position, velocity and flight time

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BibTeXRIS

1967-01-01. Interplanetary guidance system requirements study. Volume 2 - Computer program descriptions. Part 9 - Program description for optimum low thrust trajectories. https://ntrs.nasa.gov/citations/19680002381

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