An optimal, analytic solution to the linear- gravity, constant-thrust trajectory problem
- 1 July 1971
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Spacecraft and Rockets
- Vol. 8 (7), 793-796
- https://doi.org/10.2514/3.30320
Abstract
No abstract availableKeywords
This publication has 1 reference indexed in Scilit:
- A closed-form solution for minimum-fuel, constant-thrust trajectoriesAIAA Journal, 1970