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
1979
22 pages
Report
Keine Angabe
Englisch
SERT II 1979 Extended Flight Thruster System Performance
AIAA | 1981
|SERT II 1979 extended flight thruster system performance
NTRS | 1979
|SERT II 1979 extended flight thruster system performance
AIAA | 1979
|SERT 2 1979 extended flight thruster system performance
NTRS | 1979
|SERT II 1980 extended flight thruster experiments
AIAA | 1981
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