Effects of Postpulse Surface Temperature on Micropulsed Plasma Thruster Operation
Author:
Affiliation:
1. University of Illinois at Urbana–Champaign, Urbana, Illinois 61801
2. W.E. Research, Rosamond, California 93560
3. U.S. Air Force Research Laboratory, Kirtland Air Force Base, New Mexico 87117
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/10.2514/1.13032
Reference16 articles.
1. AFRL MicroPPT Development for Small Spacecraft Propulsion
2. Propellant Losses Because of Particulate Emission in a Pulsed Plasma Thruster
3. Herriott Cell augmentation of a quadrature heterodyne interferometer
4. Effect of Propellant Temperature on Efficiency in the Pulsed Plasma Thruster
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