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Plasma Deflection and Detachment Methods in a Pulsed Magnetic Field

Completed TRL 3 (started at 2, targeting 3)

Description

The approach is experimental demonstration at the university of alabama Huntsville.

Benefits

Goal is validation of pulsed magnetic nozzle performance relevant to the Pulsed Fission-Fusion propulsion system.

Details

Technology areaPropulsion Systems > Electric Space Propulsion > Electrothermal Propulsion
ProgramCenter Innovation Fund: MSFC CIF (MSFC CIF)
Lead organizationMarshall Space Flight Center, Huntsville, AL
Start date2018-10-01
End date2019-09-30

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