Satellite Platform CubeSat 3U for Complex Missions
Glavkosmos
A 3U CubeSat platform designed for complex space missions like remote sensing, featuring a 3-axis orientation and stabilization system and GaAs solar panels.
Key figurescomparable across the catalogue
- Power
- 2 W
- Largest dimension
- 340.5 mm
- Design life
- 1 years
- Lead time
- 9 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
- 2018
- Design life
- 1 years
- Lead time
- 9 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, months, not less than
- 6 months
- Dimensions
- 108 × 108 × 340.5 mm
- Mass (assembled, w/o payload) kg, not more than
- 2 kg
- Available space for payload
- 80*70*120 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, w, not less than
- 2 W
- Transmitter power
- 1 W
- Radiochannel speed, half-duplex
- 9600 bps
About
The Satellite Platform CubeSat 3U for Complex Missions is a fully assembled, verified, and tested satellite platform. It is specifically designed for use in complex space missions, such as remote sensing, due to its integrated 3-axis orientation and stabilization system and high-efficiency GaAs solar panels. The platform was released in 2018 and offers a guaranteed service life of 1 year, with an estimated production and delivery time of 9 months. While flight qualification is not stated, the product can be adapted to customer requirements. Payload integration is possible before final tests. The platform is designed for Low Earth Orbit (LEO) up to 650 km and has an active lifetime of at least 6 months. It has dimensions of 108x108x340.5 mm and a mass of no more than 2 kg (assembled, without payload). It provides an available space for payload of 80x70x120 mm, an accumulator capacity of at least 39 W*h, and an available average power consumption for the payload of at least 2 W per orbit. The on-board interface is CAN2.0 B. The platform includes a 1W transmitter with a radio channel speed of 9600 bps (half-duplex). The complete package includes 12 side GaAs solar panels with coils, 2 end edge GaAs solar panels with coils, a power supply system with a battery unit, a motherboard with an ADCS controller, a UHF transceiver, a 3U CubeSat structure, 6 protective covers, a UHF antenna with a service panel, a charger, and a transportation case for 3U.
Documentation
No public datasheet yet — request the datasheet / ICD from the supplier.