Dual Mode Operation of a Hydromagnetic Plasma Thruster to Achieve Tunable Thrust and Specific Impulse
T.C. Underwood, W. Riedel, M.A. Cappelli

TL;DR
This study introduces a pulsed hydromagnetic plasma thruster capable of dual mode operation with tunable thrust and specific impulse, demonstrated with nitrogen propellant, suitable for low Earth orbit applications.
Contribution
The paper presents the first demonstration of a hydromagnetic plasma thruster with switchable modes based on propellant flow dynamics, enabling adjustable performance parameters.
Findings
Exhaust velocities range from 10 km/s to 55 km/s.
Specific impulse varies from 2600 to 5600 seconds.
Thrust reaches up to 31 mN in burst mode.
Abstract
We report here on initial studies of a pulsed hydromagnetic plasma gun that can operate in either a pre-filled or a gas-puff mode on demand. These modes enable agile and responsive performance through tunable thrust and specific impulse. Operation with a molecular nitrogen propellant is demonstrated to show that the hydromagnetic thruster is a candidate technology for air-harvesting and drag compensation in very low Earth orbit. Dual mode operation is achieved by leveraging propellant gas dynamics to change the fill fraction and flow collisionality within the thruster. This results in the formation of distinct modes that are characterized by the current-driven hydromagnetic waves that they allow, namely a magneto-deflagration and magneto-detonation respectively. These modes can be chosen by changing the time propellant is allowed to diffuse into the thruster based on the desired…
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Taxonomy
TopicsPlasma Diagnostics and Applications · Ionosphere and magnetosphere dynamics · Astro and Planetary Science
