SERVIS-1, or Space Environment Reliability Verification Integrated System 1, is a Japanese satellite designed for testing the performance of commercial off-the-shelf products in the space environment. It has a mass of about 840 kg, and was launched on 30 October 2003 from the Plesetsk Cosmodrome by Eurockot, who used a Rokot rocket with a Briz-KM upper stage. The satellite was active for two years.[3] A second satellite, SERVIS-2, was launched in 2010.
Experiments
Nine experiments were being conducted by SERVIS-1.[3]
| Name | Full name | Description | Remarks |
|---|---|---|---|
| VTS | Vane-type Propellant Tank System | ||
| INU | Integrated Navigation Unit | ||
| PCDS | Power Control and Distribution Unit | ||
| APDM | Advanced Paddle Drive Mechanism | ||
| ATTC | Advanced Tracking Telemetry and Command Transponder | ||
| OBC | On Board Computer | ||
| SIS | Integrated Satellite Controller with Star Sensor | ||
| LIB | Lithium Ion Battery System | ||
| FOIRU | Fibre Optic Gyro Inertial Reference Unit |
Results from the mission
All the modules on the satellite worked as planned.[4] The mission tested a number of electronic components, and determined that the rate of single-event upsets at its 1000 km orbit was substantially less than had been expected from tests using heavy ion bombardment on the ground.[3]
See also
References
- ^ McDowell, Jonathan. “Launch Log”. Jonathan’s Space Page. Retrieved 2 June 2010.
- ^ a b c McDowell, Jonathan. “Satellite Catalog”. Jonathan’s Space Page. Retrieved 2 June 2010.
- ^ a b c “PROJECT_SERVIS”. Archived from the original on 2012-03-07.
- ^ “On-orbit Operation of SERVIS-1”. Archived from the original on 2012-03-13.