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Experimental Evaluation of the T100-3 Stationary Plasma Thruster and Xenon Propellant System For The RHETT-1 ProgramA 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. ...
Document ID
20210004974
Acquisition Source
Jet Propulsion Laboratory
Document Type
Other
External Source(s)
hdl:2014/26048
Authors
Petrosov, V.
Lasinsky, M.
Vasin, A.
Mueller, J.
Garner, C. E.
Date Acquired
July 1, 1996
Publication Date
July 1, 1996
Publication Information
Publisher: UNKNOWN
Distribution Limits
Public
Copyright
Other
Technical Review
Keywords
T100-3
Stationary
Plasma
Thruster
xenon
propellant
system
RHETT-1
program
Russian
Hall
plasma
thruster
plasma
thruster
xenon
propellant
subsytem
Lewis
Research
Center

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