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

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dc.contributor.author Garner, C. E. en_US
dc.contributor.author Mueller, J. en_US
dc.contributor.author Vasin, A. en_US
dc.contributor.author Lasinsky, M. en_US
dc.contributor.author Petrosov, V. en_US
dc.date.accessioned 2004-09-30T22:25:34Z
dc.date.available 2004-09-30T22:25:34Z
dc.date.issued 1996-07-01 en_US
dc.identifier.citation Orlando, Florida, USA en_US
dc.identifier.clearanceno 96-1064 en_US
dc.identifier.uri http://hdl.handle.net/2014/26048
dc.description.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. ... en_US
dc.format.extent 2753571 bytes
dc.format.mimetype application/pdf
dc.language.iso en_US
dc.subject.other T100-3 Stationary Plasma Thruster xenon propellant system RHETT-1 program Russian Hall plasma thruster plasma thruster xenon propellant subsytem Lewis Research Center en_US
dc.title Experimental Evaluation of the T100-3 Stationary Plasma Thruster and Xenon Propellant System For The RHETT-1 Program en_US


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