CubeSat ADCS Testing Facility
- Purpose: Designed for functional testing of CubeSat 3U orientation and stabilization system.
- Year of release: 2014
- Guaranteed service life (years): _
- Estimated production / delivery time (months): 6
- Flight qualification of the product: No
- Possibility to adapt the product to customer requirements: No
Parameter | Value |
---|---|
Dimensions of test bench, mm, not less than | 5000х3000х2500 |
Mass, kg, not less than | 250 |
Power voltage, V | 220 |
Computer processor frequency, GHz | 3 |
RAM capacity, Gb, not less than | 4 |
Video card, Gb, not less | 1 |
Hard disk, Gb, not less | 500 |
Screen, difinition, not worse | 1920х1080 |
Balancing system | manual |
Contents:
- air bearing 15 kg - 1 pc.;
- platform for installation of the satellite CubeSat 3U - 1 pc.;
- sun simulator (halogen) - 1 pc.;
- magnetic field simulator - 1 pc.;
- automatized working place - 1 pc.;
- autonomous measurements system - 1 pc.
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