SERVIS-1
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
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| | | Payloads are separated by bullets ( · ), launches by pipes ( | ). Manned flights are indicated in bold text. Uncatalogued launch failures are listed in italics. Payloads deployed from other spacecraft are denoted in brackets. |
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