Satellite Platform CubeSat 1U
Glavkosmos
A 1U CubeSat platform designed for scientific and educational missions, featuring an integrated power supply, onboard computer, UHF transceiver, and flight heritage.
Key figurescomparable across the catalogue
- Power
- 0.25 W
- Largest dimension
- 113 mm
- Design life
- 1 years
- Lead time
- 5 months
Normalised to common units so this product can be compared with others in its category. The supplier's own wording is below.
As published by the supplier
- Purpose
- Designed for scientific and educational missions.
- Year of release
- 2018
- Design life
- 1 years
- Lead time
- 5 months
- 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
- Yes
- Target orbit
- LEO up to 650 km
- Active lifetime, months, not less than
- 6 months
- Dimensions
- 108 × 108 × 113 mm
- Mass (assembled, w/o payload) kg, not more than
- 0.9 kg
- Available space for payload
- 80*70*20 mm
- Accumulator capacity, w*h, not less than
- 39 W*h
- On-board interface
- CAN2.0 B
- Available average power consumption of payload per orbit, mw, not less than
- 250 mW
- Transmitter power
- 1 W
- Radiochannel speed, half-duplex
- 9600 bps
About
The Satellite Platform CubeSat 1U is a fully assembled, verified, and tested satellite platform designed for scientific and educational missions. Released in 2018, it offers a guaranteed service life of 1 year and an estimated production/delivery time of 5 months. The platform is flight qualified, having flown as part of the SiriusSat-1.2 satellites launched on August 15, 2018. It can be adapted to customer requirements. The platform is designed for Low Earth Orbit (LEO) up to 650 km and has an active lifetime of at least 6 months. It provides 80x70x20 mm of available space for payload integration and an accumulator capacity of at least 39 W*h. The onboard interface is CAN2.0 B, and it can supply an average power consumption of at least 250 mW to the payload per orbit. The platform includes a 1W transmitter with a radio channel speed of 9600 bps (half-duplex). The complete package includes four side Si solar panels with coils, two end edge Si solar panels with coils, a power supply system with a battery unit, a motherboard, an onboard computer, a UHF transceiver, the 1U CubeSat structure, six protective covers, a UHF antenna with a service panel, a charger, and a transportation case for 1U. Payload integration is possible before testing.
Documentation
No public datasheet yet — request the datasheet / ICD from the supplier.