Description
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OrbiCraft-Pro satellite kit presents a set of onboard devices of CubeSat-compliant spacecraft. When assembled, it can operate in laboratory and in open space conditions as well. Design supports both ways of usage: in a laboratory for educational purposes and on low-Earth orbits as CubeSat satellite for scientific purposes.
“Profi” modification* is assembled, verified, fully tested flight unit with installed and calibrated 3-axis orientation system and GaAs solar panels.
Contents:
- 3U CubeSat structure – 1 pc.
- On-board computer – 1 pc.
- Power supply unit – 1 pc.
- GaAs solar panel (side) – 12 pcs.
- GaAs solar panel (edge) – 2 pcs
- UHF transceiver – 1 pc.
- UHF antenna system with service panel and RBF – 1 pc.
- Reaction wheels module with 4 wheels - 1 pc.
- Sun sensors – 6 pcs.
- ADCS controller option for OBC - 1 pc.
- Payload development kit
- Protection side panels 3U – 4 pcs.
- Protection edge panels 3U – 2 pcs.
- Connection wires set 3U
- Transportation case
- USB-cable
- Charger
Options included:
- Assembling and verification on manufacturer site
- Set of GaAs solar panels
- 3-axis orientation system including 6 sun sensors
- Basic functional testing with protocol: PSU cycling, radio channel, electromagnetic angular velocity damping test
- Space qualification tests with approved protocol: vacuum, thermal and mechanical impact tests
- Payload development kit
*Standard modification. Can be changed for particular project.
Mass assembled (w/o payload) | 1,45 kg |
Max mass allowed (w/ payload) | 4 kg |
Dimensions (w/ springs pressed and antenna folded) | 108x108x340.5 mm |
Dimensions at rails (w/ deployment system pressed) | 100х100x340.5 mm |
Available volume for payload | not less than 80х70х140 mm |
Output voltage | 5V ±0.5 V |
Output voltage consumption | not more than 2A |
Available average power consumption of payload on LEO | not more than (to be precised for exact orbit) 1500 mW |
Battery capacity | not less than 39 Wh |
On-board interface | CAN2.0 B |
Number of solar panels | 14 pcs. |
Peak capacity made by one solar panel on LEO | not less than 2 W |
Operating temperature range | -30...+60 °С |
Telemetry transmitte | digital beacon with systems and payload status. Regular and rich telemetry of systems by timer. Service telemetry on request. |
Radio channel frequency | 435-437 MHz, frequency modulation |
Radio channel protocol | AX.25, FEC |
Radio data | rate 4800 bit/s, 56700 bit/s (default) |
Battery type | Li-Ion 2S 5000 mAh |
Battery rated voltage | 7.4 V |
Max. Battery Charging Current | 5A |