Publisher
American Institute of Aeronautics and Astronautics
Reference13 articles.
1. Optimal Nonplanar Escape from Circular Orbits
2. Four-Body Trajectory Optimization
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4. 5Webb, E. D. "A Preliminary Analysis of a Three-Impulse Technique for Transearth Injection from Highly Inclined Orbits," Tech. Rep. LMSC/A822605, Lockheed Missiles and Space Company, Sunnyvale, California, May 1966.
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