Satellite Platform CubeSat 1U
A 1U CubeSat platform designed for scientific and educational missions, featuring an integrated power supply, onboard computer, UHF transceiver, and flight heritage.
Typed specifications8 values
Discloses 3 of 7 fields engineers filter by in this category (category median 3).
- Mass
- 900 g product page
- Envelope (L×W×H)
- 108 × 108 × 113 mm product page
- Power consumption
- 0.25 W product page 1 W
- Design lifetime
- 1 years product page
- Lead time
- 5 months product page
- Form factor
- 1U from product name · product page
- Orbit
- LEO product page
Each value is typed with its unit and measurement condition and cites the datasheet page it was taken from. Nothing is guessed: a field that is absent here has not been published by the manufacturer. machine-extracted ✓ checked by NewSpace Market ✓ manufacturer confirmed by the manufacturer.
As published by the supplier17 lines, in the manufacturer's own wording
- 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.