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The interactions of solar arrays with electric thrustersThe generation of a charge-exchange plasma by a thruster, the transport of this plasma to the solar array, and the interaction of the solar array with the plasma after it arrives are all described. The generation of this plasma can be described accurately from thruster geometry and operating conditions. The transport of the charge-exchange plasma was studied experimentally with a 15 cm thruster. A model was developed for simple thruster-array configurations. A variety of experiments were surveyed for the interaction of the plasma at the solar array.
Document ID
19770030171
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Kaufman, H. R.
(Colorado State Univ. Fort Collins, CO, United States)
Isaacson, G. C.
(Colorado State University Fort Collins, Colo., United States)
Domitz, S.
(NASA Lewis Research Center Cleveland, Ohio, United States)
Date Acquired
August 9, 2013
Publication Date
November 1, 1976
Subject Category
Spacecraft Propulsion And Power
Report/Patent Number
AIAA PAPER 76-1051
Meeting Information
Meeting: International Electric Propulsion Conference
Location: Key Biscayne, FL
Start Date: November 14, 1976
End Date: November 17, 1976
Sponsors: American Institute of Aeronautics and Astronautics
Accession Number
77A13023
Funding Number(s)
CONTRACT_GRANT: NSG-3038
Distribution Limits
Public
Copyright
Other

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