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NASA NTRS ยท 20080033025

Magnetohydrodynamic Augmented Propulsion Experiment

Abstract

Over the past several years, efforts have been under way to design and develop an operationally flexible research facility for investigating the use of cross-field MHD accelerators as a potential thrust augmentation device for thermal propulsion systems. The baseline configuration for this high-power experimental facility utilizes a 1.5-MWe multi-gas arc-heater as a thermal driver for a 2-MWe MHD accelerator, which resides in a large-bore 2-tesla electromagnet. A preliminary design study using NaK seeded nitrogen as the working fluid led to an externally diagonalized segmented MHD channel configuration based on an expendable heat-sink design concept. The current status report includes a review of engineering/design work and performance optimization analyses and summarizes component hardware fabrication and development efforts, preliminary testing results, and recent progress toward full-up assembly and testing

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BibTeXRIS

Litchford, Ron J.. 2008-05-30. Magnetohydrodynamic Augmented Propulsion Experiment. https://ntrs.nasa.gov/citations/20080033025

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