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Experimental Evaluation of the T100-3 Stationary Plasma Thruster and Xenon Propellant System For The RHETT-1 Program

Experimental Evaluation of the T100-3 Stationary Plasma Thruster and Xenon Propellant System For The RHETT-1 Program

Garner, C. E.; Mueller, J.; Vasin, A.; Lasinsky, M.; Petrosov, V.
URI: http://hdl.handle.net/2014/26048
Date: 1996-07-01
Citation: Orlando, Florida, USA

Abstract:

A T-100-3 Russian Hall plasma thruster, xenon flow control unit (XFCU) and US xenon propellant subsystem developed for the RHETT-1 propulsion system are described. The propellant system includes a pressure regulator, on/off valves, service valve and high/low pressure transducers, built to flight-like standards and assembled onto a mounting plate structure. ...

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