VX-200 Magnetoplasma Thruster Performance Results Exceeding Fifty-Percent Thruster Efficiency
Author:
Affiliation:
1. Ad Astra Rocket Company, Webster, Texas 77598
2. University of Houston, Houston, Texas 77204
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Space and Planetary Science,Mechanical Engineering,Fuel Technology,Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.B34085
Reference36 articles.
1. SP-100 nuclear electric propulsion for Mars cargo missions
2. A Survey of Propulsion Options for Cargo and Piloted Missions to Mars
3. Helicons-the early years
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