Mission Analysis for CubeSats with Micropropulsion
Author:
Affiliation:
1. Western Michigan University, Kalamazoo, Michigan 49008
2. Jet Propulsion Laboratory, California Institute of Technology, Pasadena, California 91109
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.A33564
Reference36 articles.
1. KleshA.KrajewskiJ. “CubeSats to Mars in 2016,” Proceedings of the 29th AIAA/USU Conference on Small Satellites, SSC15-III-3, Logan, UT, 2015.
2. FrostC. “Small Spacecraft Technology State of the Art,” NASA Ames Research Center NASA/TP-2014-216648/rev1, 2014.
3. Mission Capability Assessment of CubeSats Using a Miniature Ion Thruster
4. Mission Applications of the MRS-142 CubeSat High-Impulse Adaptable Monopropellant Propulsion System (CHAMPS)
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