Theoretical Design of a Magnetic-Nozzle Acceleration System for Fusion Propulsion
- Author(s):
- Mikellides, I.G. ( The Ohio State University )
- Mikellides, P.G.
- Turchi, P.J.
- York, T.M.
- Publication title:
- AIAA paper
- Title of ser.:
- AIAA Paper : AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit
- Ser. no.:
- 2000
- Pub. Year:
- 2000
- No.:
- 2000-3367
- Paper no.:
- 00-3367
- Page(from):
- 1
- Page(to):
- 13
- Pub. info.:
- American Institute of Aeronautics and Astronautics
- ISSN:
- 01463705
- Language:
- English
- Call no.:
- A07400
- Type:
- Technical Paper
Similar Items:
American Institute of Aeronautics and Astronautics |
7
Technical Paper
Modeling of Magnetically-Guided Plasma Flows Form a Gigawatt-Level Magnetoplasmadynamic Source.
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
8
Technical Paper
Progress on the Godzilla Gigawatt MPD Plasma Accelerator and Nozzle for Fusion Propulsion Simulations
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 |
11
Technical Paper
Development of equation-of-state and transport properties for molecular plasmas in pulsed plasma thrusters, part II: a two-temperature equation of state for …
American Institute of Aeronautics and Astronautics |
6
Technical Paper
EXPERIMENTAL AND THEORETICAL INVESTIGATION OF AN INVERSE-PINCH COAXIAL PULSED PLASMA THRUSTER
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |