Modeling of Ablation-Fed Pulsed Plasma Thruster Operation Using a New Approach to the Ablation Process

Author:

Henrikson Erik,Mikellides Pavlos

Publisher

American Institute of Aeronautics and Astronautics

Reference14 articles.

1. 1Mikellides, P. G. and Turchi, P. J. “Modeling of late-time ablation in Teflon pulsed plasma thrusters,” 32nd AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit, Lake Buena Vista, FL, July 1996.

2. 2Keefer, D. R. and Rhodes, R. “Electromagnetic Acceleration in Pulsed Plasma Thrusters,” Proceedings of the 25th International Electric Propulsion Conference, The Electric Rocket Propulsion Society, Worthington, OH, 1997, pp.229-236.

3. Numerical Modeling of a Pulsed Electromagnetic Plasma Thruster Experiment

4. 4Pencil, E. and Kamhawi, H. “Alternate Propellant Evaluation for 100-joule-class Pulsed Plasma Thrusters,” 39th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit, Huntsville, AL, July 2003.

5. 5Henrikson,E.M.andMikellides,P.G.“ExperimentalAssessmentofaBenchmarkAblation-fedPulsedPlasmaThruster,” 43rd AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit, Cincinnati, OH, July 2007.

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