Ulysses, one year after the launch
Abstract
Ulysses is currently one year underway in a huge heliocentric orbit. A late change in some of the blankets' external material was required to prevent electrical charging due to contamination by nozzle outgassing products. Test results are shown, governing various ranges of plasma parameters and sample temperatures. Even clean materials show a few volts charging due to imperfections in the conductive film. Thermal environment in the Shuttle cargo bay proved to be slightly different from prelaunch predictions: less warm with doors closed, and less cold with doors opened. Temperatures experienced in orbit are nominal. A problem was caused by a complex interaction of a Sun induced thermal gradient in a sensitive boom on the dynamic stability of the spacecraft. A user interface program was an invaluable tool to ease computations with the mathematical models, eliminate error risk and provide configuration control.
- Publication:
-
ESA Special Publication
- Pub Date:
- December 1991
- Bibcode:
- 1991secs.conf..951P
- Keywords:
-
- Electrostatic Charge;
- Mathematical Models;
- Solar Blankets;
- Spacecraft Performance;
- Spacecraft Temperature;
- Temperature Control;
- Ulysses Mission;
- Contamination;
- Dynamic Stability;
- Films;
- Launching;
- Spacecraft Design, Testing and Performance