Operational Characteristics of a Low-Energy FARAD Thruster
Author:
Publisher
American Institute of Aeronautics and Astronautics
Reference5 articles.
1. Faraday Acceleration with Radio-Frequency Assisted Discharge
2. 2K.A.Polzin,M.F.Rose,andR.Miller, "Laboratory-Model Integrated-SystemFARADThruster," 44thAIAA/ASME/SAE/ASEEJointPropuls. Conf., Hartford, CT,July 2008. AIAA Paper 2008-4821.
3. Axial propagation of helicon waves
4. Instantaneous Direct‐Display System of Plasma Parameters by Means of Triple Probe
5. Performance optimization criteria for pulsed inductive plasma acceleration
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