Extremal Rocket Motion with Maximum Thrust in a Linear Central Field
Author:
Affiliation:
1. University of Texas at Austin, Austin, Texas 78712
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Space and Planetary Science,Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/2.3744
Reference9 articles.
1. Analytic solutions for intermediate-thrust arcs of rocket trajectories in a Newtonian field
2. Ehricke, K. A., Space Flight, Volume 2, Dynamics, Van Nostrand, New York, 1962, pp.498-504.
3. On an analytical solution of the optimum trajectory problem in a gravitational field
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