| タイトル | The Evolution of the VASIMR Engine |
| 本文（外部サイト） | http://hdl.handle.net/2060/20100033244 |
| 著者（英） | Nguyen, Tri X.; Squire, Jared P.; Chang-Diaz, F. R.; Petro, Andrew |
| 著者所属（英） | NASA Johnson Space Center |
| 発行日 | 2001-08-28 |
| 言語 | eng |
| 内容記述 | Our future deep space explorers face many daunting challenges but three of these loom high above the rest: Physiological debilitation, radiation sickness and psychological stress. Many countermeasures are presently being considered to ameliorate these difficulties however, in the long run, two important new developments are required: abundant space power and advanced propulsion. The development of the Variable Specific Impulse Magnetoplasma Rocket (VASIMR) addresses these important areas of need. The VASIMR is a high power, radio frequency-driven magneto plasma rocket, capable of very high exhaust velocities. In addition, its unique architecture allows in-flight mission-optimization of thrust and specific impulse to enhance performance and reduce trip time. A NASA-led, research team, involving industry, academia and government facilities is pursuing the development of this concept in the United States. The technology can be validated, in the near term, in venues such as the International Space Station, where it can also serve as both a drag compensation device and a plasma contactor for the orbital facility. Other near-Earth applications in the commercial and scientific satellite sectors are also envisioned. This presentation covers the present status of the technology, plans for its near term deployment and a vision for its future evolution. |
| NASA分類 | Spacecraft Propulsion and Power |
| レポートNO | JSC-CN-7092 |
| 権利 | No Copyright |
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