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Performance Evaluation and Life Testing of the SPT-100A cyclic endurance test of the Russian 1.35 kW Stationary Plasma Thruster SPT-100 is described.
Document ID
20060039356
Acquisition Source
Jet Propulsion Laboratory
Document Type
Preprint (Draft being sent to journal)
External Source(s)
hdl:2014/35856
Authors
Garner, Charles E.
Polk, James C.
Goodfellow, Keith M.
Pless, Lewis C.
Brophy, John R.
Date Acquired
August 23, 2013
Publication Date
September 13, 1993
Subject Category
Spacecraft Propulsion And Power
Distribution Limits
Public
Copyright
Other
Keywords
SPT-100 thrusters propulsion performance life testing Russian evaluation

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