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Experimental performance of a low-thrust, divergent-flow, Contact-ionization electrostatic thrustor.Low thrust divergent flow cesium-on-tungsten contact ionization electrostatic thrustor for satellite attitude control and stationkeeping missions
Document ID
19660057761
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Lathem, W. C.
Staggs, J. F.
Date Acquired
August 3, 2013
Publication Date
June 1, 1966
Subject Category
Propulsion Systems
Report/Patent Number
AIAA PAPER 66-569
Report Number: AIAA PAPER 66-569
Accession Number
66A37051
Distribution Limits
Public
Copyright
Other
Keywords
ION ENGINE
FLOW DEFLECTION
SATELLITE ATTITUDE CONTROL
CESIUM ION

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