Trajectory Options for Manned Mars Missions
Author:
Affiliation:
1. Pratt and Whitney Aircraft, United Technologies Corporation, East Hartford, Connecticut 06108
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Space and Planetary Science,Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/1.9770
Reference16 articles.
1. 1Von Braun, W., The Mars Project, Univ. of Illinois Press, Urbana, IL, 1953(reprinted in 1991), pp.38-64.
2. Nuclear thermal propulsion vehicle design for the Mars flyby with surface exploration mission
3. 3Zubrin, R. M., The Case for Mars, Simon and Schuster, New York, 1996, pp.75-84.
4. Mars direct - A simple, robust, and cost effective architecture for the Space Exploration Initiative
5. How shall we go to Mars? A review of mission scenarios
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