Optimal aerodynamic-propulsive maneuvering for the orbital plane change of a space vehicle.
- 1 December 1967
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Spacecraft and Rockets
- Vol. 4 (12) , 1678-1680
- https://doi.org/10.2514/3.29156
Abstract
No abstract availableKeywords
This publication has 3 references indexed in Scilit:
- Implications of maneuvering-range constraints on lifting-vehicle design.Journal of Spacecraft and Rockets, 1967
- Combined aerodynamic-propulsive orbital plane change maneuverAIAA Journal, 1965
- Change of Satellite Orbit Plane by Aerodynamic ManeuveringJournal of the Aerospace Sciences, 1962