Direct-drive concept based on CDL capacitor technology powring a thruster with anode layer
- Author(s):
- Hrbud, Ivana ( Space Power Institute, Auburn University )
- Rose, M. Frank
- Publication title:
- AIAA paper
- Title of ser.:
- AIAA Paper : Aerospace Sciences Meeting and Exhibit
- Ser. no.:
- 1997
- Pub. Year:
- 1997
- No.:
- 97-1007
- Paper no.:
- 97-1007
- Page(from):
- 1
- Page(to):
- 14
- Pub. info.:
- American Institute of Aeronautics and Astronautics
- ISSN:
- 01463705
- Language:
- English
- Call no.:
- A07400
- Type:
- Technical Paper
Similar Items:
1
Technical Paper
Integrating CDL capacitor technology in the power supply of a thruster with anode layer
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
2
Technical Paper
TAL performance and mission analysis in a CDL capacitor powered direct-drive configuration
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
3
Technical Paper
Performance of a multilayer ceramic capacitor power system for pulsed plasma thrusters
American Institute of Aeronautics and Astronautics |
9
Technical Paper
Final Report: Thermal Storage Advanced Thruster System (TSATS) Experimental Program
National Aeronautics and Space Adminstration |
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
6
Technical Paper
Assessment of High-Voltage Solar Array Concepts for a Direct Drive Hall Effect Thruster System
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |