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Title: Experimental Evaluation of the T100-3 Stationary Plasma Thruster and Xenon Propellant System For The RHETT-1 Program
Authors: Garner, C. E.
Mueller, J.
Vasin, A.
Lasinsky, M.
Petrosov, V.
Issue Date: 1-Jul-1996
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. ...
Appears in Collections:JPL TRS 1992+

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