Orbital Motion Under Continuous Tangential Thrust
- 1 November 1992
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Guidance, Control, and Dynamics
- Vol. 15 (6) , 1503-1507
- https://doi.org/10.2514/3.56583
Abstract
No abstract availableThis publication has 3 references indexed in Scilit:
- Rocket trajectory optimization - 1950-1963Journal of Guidance, Control, and Dynamics, 1991
- Escape From a Circular Orbit Using Tangential ThrustJournal of Jet Propulsion, 1958
- Take-Off from Satellite OrbitJournal of the American Rocket Society, 1953