Satellite Platform CubeSat 6U
Glavkosmos
A 6U CubeSat satellite platform designed for complex space missions, featuring a 3-axis orientation and stabilization system, GaAs solar panels, and an integrated power supply, ADCS controller, and communication systems.
Key figurescomparable across the catalogue
- Power
- 4 W
- Largest dimension
- 340.5 mm
- Design life
- 1 years
- Lead time
- 14 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
- Can be used in complex space missions (f.e. Remote sensing) because contains 3-axis orientation and stabilization system, and GaAs solar panels.
- Year of release
- 2019
- Design life
- 1 years
- Lead time
- 14 months
- Flight qualification of the product
- No
- Possibility to adapt the product to customer requirements
- Yes
- Target orbit
- LEO up to 650 km
- Active lifetime, years, not less than
- 1
- Dimensions
- 108 × 221 × 340.5 mm
- Mass (assembled, w/o payload) kg, not more than
- 5 kg
- Available space for payload
- 90 × 90 × 300 mm
- Accumulator capacity, w*h, not less than
- 78 W*h
- On-board interface
- CAN2.0 B
- Available average power consumption of payload per orbit, w, not less than
- 4 W
- Radiochannel speed, half-duplex
- 9600 bps
- Transmission speed (x-band), simplex, mbps, not less than
- 10 Mbps
About
The Satellite Platform CubeSat 6U is a fully assembled, verified, and tested satellite platform intended for complex space missions, such as remote sensing. It incorporates a 3-axis orientation and stabilization system and GaAs solar panels for robust operation in orbit. The platform was released in 2019 and offers a guaranteed service life of at least 1 year. The estimated production and delivery time is 14 months. While it does not have flight qualification, the product can be adapted to customer requirements. The platform includes 18 side GaAs solar panels with coils, 4 end edge GaAs solar panels with coils, a power supply system with a battery unit, a motherboard with an ADCS controller, a computer, a UHF transceiver, the 6U CubeSat structure, 6 protective covers, a UHF antenna with a service panel, a charger, a transportation case for 6U, and an X-band transmitter. Payload integration is possible before testing.
Documentation
No public datasheet yet — request the datasheet / ICD from the supplier.