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ATS-6 - Cesium bombardment engine north-south stationkeeping experimentTwo 0.004 N thrust cesium bombardment ion thrustors have been developed and used for north-south stationkeeping in the geostationary Applications Technology Satellite-6 (ATS-6). The thrustor subsystems are mounted on the north and south faces of the earth viewing module such that 0.0026 N of thrust is applied normal to the orbit plane and 0.0036 N is applied radially upward. The change in the orbit inclination of the satellite is maintained at zero by operating the two thrustors alternately so that their thrust components, normal to the orbital plane, are symmetrically applied about the nodal crossings. Initial operation of the thrustors was successful. There was no interference with the satellite communications systems and the predicted spacecraft operating potential was verified. Subsequent trials failed due to a defect in the operation of the propellant reservoirs in zero g. A feed line valve is under development to correct this difficulty.
Document ID
19760034957
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Worlock, R. M.
(NASA Goddard Space Flight Center Greenbelt, MD, United States)
James, E. L.
(Xerox Electro-Optical Systems Pasadena, Calif., United States)
Hunter, R. E.
(NASA Goddard Space Flight Center Greenbelt, MD, United States)
Bartlett, R. O.
(NASA Goddard Space Flight Center Greenbelt, Md., United States)
Date Acquired
August 8, 2013
Publication Date
November 1, 1975
Publication Information
Publication: IEEE Transactions on Aerospace and Electronic Systems
Volume: AES-11
Subject Category
Spacecraft Propulsion And Power
Accession Number
76A17923
Distribution Limits
Public
Copyright
Other

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