Report of the Seasat Failure Review Board
Abstract
The Seasat spacecraft failed on October 9, 1978, after satisfactory operation in orbit for 105 days, as a result of a loss of electrical power in the Agena bus that was used as a part of the spacecraft. The loss of power was caused by a massive and progressive short in one of the slip ring assemblies that was used to connect the rotating solar arrays into the power subsystem. The most likely cause of this short was the initiation of an arc between adjacent slip ring brush assemblies. The triggering mechanism of this arc could have been either a wire-to-brush assembly contact, a brush-to-brush contact, or a momentary short caused by a contaminant that bridged internal components of opposite electrical polarity.
- Publication:
-
Readings in Systems Engineering
- Pub Date:
- 1993
- Bibcode:
- 1993rse..nasa..201.
- Keywords:
-
- Agena Rocket Vehicles;
- Failure;
- Losses;
- Seasat Satellites;
- Wiring;
- Brushes;
- Contaminants;
- Polarity;
- Rotation;
- Solar Arrays;
- Spacecraft Design, Testing and Performance