Structure 1U CubeSat with Separation System
- Purpose: The structure provides simple and fast assemble, at the same time is durable base for the satellite with easy access to the devices inside and on the edges.
- Year of release: 2017
- Guaranteed service life (years): 3
- Estimated production / delivery time (months): 2
- Flight qualification of the product: Yes
- Brief history of flight qualification: In the composition of the satellites SiriusSat-1.2 (launched on 15.08.18.).
- Possibility to adapt the product to customer requirements: No
| Parameter | Value |
|---|---|
| Dimensions (w/ springs pressed), mm | 100 х 100 х 113.5 |
| Mass, g | 132 |
| Board stack | PC/104 |
| Operating temperature range, °С | -40...+85 |
| Storage temperature range, °С | -50..+105 |
| Mechanical vibration, g | 12 |
| Mechanical shock, g | 50 |
CubeSat 1U structure designed in accordance with CubeSat Design Specification rev.13 and supports modular satellite construction based on PC104 PCB stack with solar panels on the edges.
For container launches there is a deployment system which consists of 2 separation springs and double separation switches with interface for power supply unit.
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