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Dual mode operation of a hydromagnetic plasma thruster to achieve tunable thrust and specific impulse
Author(s) -
Thomas C. Underwood,
William Riedel,
Mark A. Cappelli
Publication year - 2021
Publication title -
journal of applied physics
Language(s) - English
Resource type - Journals
SCImago Journal Rank - 0.699
H-Index - 319
eISSN - 1089-7550
pISSN - 0021-8979
DOI - 10.1063/5.0051467
Subject(s) - propellant , specific impulse , thrust , detonation , deflagration to detonation transition , aerospace engineering , mechanics , plasma , collisionality , physics , explosive material , magnetohydrodynamic drive , impulse (physics) , propulsion , deflagration , magnetohydrodynamics , chemistry , classical mechanics , engineering , organic chemistry , quantum mechanics , tokamak

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