Satellite platform OrbiCraft-Pro 3U modification “Experimental”
SPUTNIX
An assembled and manufacturer-verified 3U CubeSat platform (article SXC3) with silicon (Si) solar panels and basic B-DOT ADCS, intended primarily as a laboratory/educational model.
Technical specifications
- Mass assembled (w/o payload)
- 1.4 kg
- Max mass allowed (w/ payload)
- 4 kg
- Dimensions (springs pressed, antenna folded)
- 108x108x340.5 mm
- Dimensions at rails
- 100x100x340.5 mm
- Available volume for payload
- not less than 80x70x140 mm
- Output voltage
- 5V +-0.5 V
- Output current
- not more than 2A
- Available average payload power on LEO
- not more than 600 mW
- Battery capacity
- not less than 39 Wh
- On-board interface
- CAN2.0 B
- Number of solar panels
- 14 pcs
- Peak power per solar panel on LEO
- not less than 0.9 W
- Operating temperature range
- -30...+60 C
- Radio channel frequency
- 435-437 MHz, FM
- Radio data rate
- 4800-56700 bit/s
- Battery type
- Li-Ion 2S 5000 mAh
- ADCS algorithms
- B-DOT
- Sensors
- Angular velocity sensor, magnetometer, temperature
About
The “Experimental” modification is an assembled/verified 3U CubeSat unit with silicon (Si) solar panels, ready for payload integration, intended primarily as a laboratory model for education. Contents: 3U CubeSat structure, on-board computer (Raspberry-Pi), power supply system with battery, twelve Si side solar panels with coils, two Si end edge solar panels with coils, UHF transceiver, UHF antenna system with service panel/RBF switch, protection panels for 3U, wiring set, transportation case, USB cable, charger, documentation. For actual missions, GaAs-panel modifications are recommended instead. Includes B-DOT ADCS algorithms and sensors: angular velocity sensor, magnetometer, and temperature sensor.
Documentation
Need the full ICD, test reports or a specific revision? Ask the supplier directly.
