Abstract
Human exploration of the Solar System would benefit greatly from substantially reduced trip-times (e.g., months vs years). To achieve the necessary high thrust-to-weight rocket at exhaust velocities optimized for fast interplanetary transfers, very hightemperature (-100 keV) plasma extracted from a thermonuclear fusion reactor would heat much larger masses of hydrogen plasma to high temperature (-100 eV). While much lower, such temperatures still require the use of magnetic fields to obtain a directed rocket exhaust. Thus, many concepts for fusion-heated rockets have development of efficient magnetic nozzles on their critical path. The Godzilla gigawatt pulser can provide a testbed for such development.
Original language | English (US) |
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State | Published - 1998 |
Externally published | Yes |
Event | 34th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit, 1998 - Cleveland, United States Duration: Jul 13 1998 → Jul 15 1998 |
Other
Other | 34th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit, 1998 |
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Country/Territory | United States |
City | Cleveland |
Period | 7/13/98 → 7/15/98 |
ASJC Scopus subject areas
- Energy Engineering and Power Technology
- Electrical and Electronic Engineering
- Mechanical Engineering
- Control and Systems Engineering
- Aerospace Engineering