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Gradient Field Imploding Liner Fusion Propulsion System

Completed TRL 3 (started at 2, targeting 3)

Description

An innovative modification to magneto-inertial fusion is proposed in which the pulsed, high current magnetic field coil and stationary central fuel target are replaced with a fast moving fusion fuel target fired axially into a static, high gradient magnetic field. As the target passes through the magnetic field gradient it effectively experiences a rapidly changing axial magnetic field, which induces strong azimuthal currents in the target liner to implode the fuel and reach fusion conditions. Among other advantages, eliminating the need to pulse the magnetic field coil allows the use of energy efficient superconducting coils in a geometry that more naturally lends itself to in-space propulsion. If successful, the proposed concept will substantially reduce Mars trip times and enable a robust architecture for human solar system exploration.

Benefits

If successful, the proposed concept will substantially reduce Mars trip times and enable a robust architecture for human solar system exploration.

Details

Technology areaPropulsion Systems > Advanced Propulsion > Solar Thermal Propulsion
ProgramNASA Innovative Advanced Concepts (NIAC)
Lead organizationMarshall Space Flight Center, Huntsville, AL
Start date2017-04-01
End date2018-01-31

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How to get involved

This is early/mid-stage (TRL 3) — 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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