Steady state tests of the thruster 2 system on the SERT 2 spacecraft are presented. A direct thrust measurement was obtained for the ion thruster during operations to increase the spacecraft spin rate to maintain spacecraft attitude stability. The continued restart tests of thruster 1 and a report on the general status of all spacecraft systems including the main solar array are presented.
SERT 2 1979 extended flight thruster system performance
Intern. Conf. on Electric Propulsion ; 1979 ; Princeton, NJ, United States
1979-01-01
Conference paper
No indication
English
SERT II 1979 Extended Flight Thruster System Performance
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|Sert 2 1979 Extended Flight Thruster System Performance
NTIS | 1979
|SERT II 1979 extended flight thruster system performance
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|SERT II 1979 extended flight thruster system performance
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