Author:
Chiravalle Vincent,Miles Richard,Choueiri Edgar
Publisher
American Institute of Aeronautics and Astronautics
Reference20 articles.
1. Development and demonstration of a 600-second mission-average I(sp) arcjet
2. 5D. J. Sullivan and M. M. Micci. Development of a microwave resonant cavity electrothermal thruster prototype. In23rdInternational Electric Propulsion Conference,Seattle, WA, September 1993. IEPC-93-036.
3. Numerical Investigation of Bluff-Body Stabilized Microwave Plasmas
Cited by
4 articles.
订阅此论文施引文献
订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献
1. A 300 W Microwave Thruster - Design and Performance Testing;40th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit;2004-06-26
2. Laser-Induced Fluorescence Measurements of a Two-Stage Microwave Electrothermal Thruster Plume;34th AIAA Plasmadynamics and Lasers Conference;2003-06-23
3. A Numerical Study of a Two-Stage Microwave Electrothermal Thruster;38th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit;2002-07-07
4. Review of the EP Activities of US Academia;38th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit;2002-07-07