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Nuclear Propulsion through Direct Conversion of Fusion Energy

Completed TRL 2 (started at 1, targeting 2)

Description

The future of manned space exploration and development of space depends critically on the creation of a vastly more efficient propulsion architecture for in-space transportation. Nuclear-powered rockets can provide the large energy density gain required. A small scale, low cost path to fusion-based propulsion is to be investigated. It is accomplished by employing the propellant to compress and heat a magnetized plasma to fusion conditions, and thereby channel the fusion energy released into heating only the propellant. Passage of the hot propellant through a magnetic nozzle rapidly converts this thermal energy into both directed (propulsive) energy and electrical energy.

Benefits

The development of this technology can enable a dramatically more efficient propulsion architecture for in-space transportation.

Details

Technology areaPropulsion Systems > Advanced Propulsion > Solar Thermal Propulsion
ProgramNASA Innovative Advanced Concepts (NIAC)
Lead organizationMSNW, LLC, Redmond, WA
Start date2011-09-01
End date2012-09-01

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This is early/mid-stage (TRL 2) — the most realistic path in is NASA SBIR/STTR, which funds small businesses and research institutions to develop technology aligned with NASA's needs (equity-free, phased funding). Check whether a current SBIR/STTR solicitation topic overlaps with this project's technology area, or contact the project directly (above) to ask.

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