Performance of Gas-Fed Pulsed Plasma Thrusters Using Water Vapor Propellant.
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American Institute of Aeronautics and Astronautics |
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Analysis of triple Langmuir probe measurements in the near-exit region of a gas-fed pulsed plasma thruster
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
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Is the Gas-Fed PPT an Electromagnetic Accelerator? An Investigation Using Measured Performance
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
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Is the gas-fed PPT an electromagnetic accelerator? An investigation using measured performance
American Institute of Aeronautics and Astronautics |
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Analysis of Triple Langmuir Probe Measurements in the Near-Exit Region of a Gas-Fed Pulsed Plasma Thruster
American Institute of Aeronautics and Astronautics |
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Pulsed Plasma Thruster Using Water Propellant, Part II: Thruster Operation and Performance Evaluation
American Institute of Aeronautics and Astronautics |