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Preliminary results in the NASA Lewis H2-O2 combustion MHD experiment

J. Marlin Smith1979NASA Technical Memorandum 79135 (E-9983); prepared for the 18th Symposium on the Engineering Aspects of Magnetohydrodynamics, Butte, Montana, June 18–20, 1979https://ntrs.nasa.gov/citations/19790014726

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Read (open NTRS PDF, loop-3 pass 41 close). Cesium-seeded H₂–O₂ combustion MHD generator in a neon-cooled cryomagnet (fields above 5 T; peak used 5 T): the combustion chamber and nozzle are water-cooled copper, 'the nozzle is designed for Mach 2 at the 4.96 cm diameter exit', stagnation pressures 5–20 atm, feeding 'a diverging circular cross section duct having an inlet Mach number of 2' of 42 copper electrodes in a Hall configuration; power output proportional to the square of the B-field; 8.74 kW (run 407) rising to 11.7 kW (run 413) when the front power takeoff moved downstream. The channel velocity is the combustor's own gas-dynamic expansion — no separate pump or compressor supplies it.

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Physical Transformation Atlas (2026). source source:smith-1979-nasa-tm-79135: Preliminary results in the NASA Lewis H2-O2 combustion MHD experiment. Dataset revision rbfbfcbb70e57 (hash of the canonical data). https://physical-transformation-atlas.wldud5192.workers.dev/source/smith-1979-nasa-tm-79135

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