Optimum Thrust Programming of Electrically Powered Rocket Vehicles in a Gravitational Field
- 1 October 1960
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in ARS Journal
- Vol. 30 (10) , 954-960
- https://doi.org/10.2514/8.5283
Abstract
No abstract availableKeywords
This publication has 4 references indexed in Scilit:
- Method for Determining Steering Programs for Low Thrust Interplanetary VehiclesARS Journal, 1959
- Interplanetary Trajectories Under Low Thrust Radical AccelerationARS Journal, 1959
- Escape From a Circular Orbit Using Tangential ThrustJournal of Jet Propulsion, 1958
- LOW-THRUST ROCKET STEERING PROGRAM FOR MINIMUM TIME TRANSFER BETWEEN PLANETARY ORBITSPublished by SAE International ,1958