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Experimental Evaluation of Russian Anode Layer ThrustersPerformance and endurance testing of a 1.35 kW thruster with anode layer (TAL), developed at the Central Research Institute of Machine Building (TsNIMASH) is described.
Document ID
20060038568
Acquisition Source
Jet Propulsion Laboratory
Document Type
Preprint (Draft being sent to journal)
External Source(s)
hdl:2014/34604
Authors
Garner, C. E.
Polk, J. E.
Brophy, J. R.
Marrese, C.
Semenkin, S.
Tverdokhlebov, S.
Date Acquired
August 23, 2013
Publication Date
June 1, 1994
Subject Category
Spacecraft Propulsion And Power
Distribution Limits
Public
Copyright
Other
Keywords
Russia stationary plasma thruster Ballistic Missile Defence Organization (BMDO)

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