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SERT II 1979 extended flight thruster system performanceThe SERT II spacecraft, launched in 1970, has been maintained in an operational, but intermittently active status since 1971. Periodic thruster status has been reported while waiting for normal orbit precession to return the spacecraft to continuous sunlight in 1979. Now, the thruster has been operated for 600 hours in the first quarter of 1979. Thruster startup and operation in 1979 is unchanged after 9 years in space. The ion thruster was gimbaled and used to maintain spin stabilization of the spacecraft. Minor components of the spacecraft have failed, but have not interfered with the functional status of the spacecraft.
Document ID
19800026216
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Kerslake, W. R.
(NASA Lewis Research Center Cleveland, OH, United States)
Ignaczak, L. R.
(NASA Lewis Research Center Cleveland, Ohio, United States)
Date Acquired
August 10, 2013
Publication Date
October 1, 1979
Subject Category
Spacecraft Propulsion And Power
Report/Patent Number
AIAA PAPER 79-2063
Report Number: AIAA PAPER 79-2063
Meeting Information
Meeting: International Electric Propulsion Conference
Location: Princeton, NJ
Start Date: October 30, 1979
End Date: November 1, 1979
Sponsors: Princeton University, AIAA, and DGLR,
Accession Number
80A10386
Distribution Limits
Public
Copyright
Other

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