Mass and Cost Model for Selecting Thruster Size in Electric Propulsion Systems

Author:

Hofer Richard,Randolph Thomas

Publisher

American Institute of Aeronautics and Astronautics

Reference28 articles.

1. Strange, N., Landau, D., Polk, J., Brophy, J., and Mueller, J. "Solar Electric Propulsion for a Flexible Path of Human Space Exploration," Presented at the61st International Astronautical Congress, IAC-10.A5.2.4, Prague, CzechRepublic, Sep.Oct.,2010.

2. Brophy, J., Strange, N., and Merrill, R. "300-kW Solar Electric Propulsion System Configuration for Human Exploration of near-Earth Asteroids," Presented at the47th Joint Propulsion Conference, (submitted for publication),SanDiego, CA,July31-Aug.3,2011.

3. Schmidt, T. D. and Auweter-Kurtz, M. "Adequate Electric Propulsion System Parameters for Piloted Mars Missions," Presented at the29th International Electric Propulsion Conference, IEPC-2009-219, Princeton, NJ, Oct.31-Nov.4,2005.

4. Flexible Piloted Mars Missions Using Continuous Electric Propulsion

5. Propulsive options for a manned Mars transportation system

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