CubeSat platform Cleon I
The Cleon platform has been designed specifically for CubeSat missions. The technology has proven itself in the Norby-1 mission - our first satellite that has been operating nominally up till now.
The reliability and versatility of the development allows to apply Cleon in a wide range of applications, such as M2M, ADS-B, AIS, remote sensing, as well as scientific research.
01
Configuration scalability from 1U to 16U
Depending on your mission objective, payload size and required power, the platform form factor can be scaled to efficiently operate the entire system and subsystems.
02
Flight heritage of the platform is over 4 years
Reliability and commitment to the cutting edge technologies are the credo of OKB Fifth Generation
03
Telemetry tracking and command meet all industry standards
Grid, our development, will allow you to download and visualize data, book satellite sessions and send control commands to your spacecrafts
04
Integration and launch support
The Cleon platform is adapted to the standards of launch operators and satellite deployer manufacturers. Before launch, our team will perform all necessary tests in the laboratory and integrate the payload at the cosmodrome
Platform specifications
1U
3U
6U
12U
Weight, w/o payload (w/ payload)
0,5 kg (1,5 kg)
3 kg (5,5 kg)
6 kg (8,5 kg)
12 kg (16 kg)
Lifetime
Not less than 1 year
Not less than 3 years
Redundancy
Partial (EPS)
Hot redundant (OBC, EPS, ADCS)
Average power available
4 – 6 W
10 – 15 W
12 – 20 W
30 – 50 W
Average power requirement or on-board systems
< 3 W
< 5 W
Battery capacity
≈ 10 A × h
≈ 15 A × h
≈ 30 A × h
Volume available for payload
0,5U (50 mm ×100 mm × 100 mm)
2U (100 mm х 100 mm х 200 mm)
5U (100 mm x 200 mm x 200 mm + 100 mm x 100 mm x 100 mm)
10U (200 mm × 200 mm × 200 mm + 100 mm x 100 mm × 200 mm)
On-board voltage and current load available for payload
3.3 V/5A; 5 V/3A; 8.4 V/2A
Orientation accuracy
< 1°
Stabilization accuracy
< 0,2°/s
Telemetry and control
UHF, S-band
Operating temperature range
-20...60 °C
1U
- Weight, w/o payload (w/ payload)
- 0,5 kg (1,5 kg)
- Lifetime
- Not less than 1 year
- Redundancy
- Partial (EPS)
- Average power available
- 4 – 6 W
- Average power requirement or on-board systems
- < 3 W
- Battery capacity
- ≈ 10 A × h
- Volume available for payload
- 0,5U (50 mm ×100 mm × 100 mm)
- On-board voltage and current load available for payload
- 3.3 V/5A; 5 V/3A; 8.4 V/2A
- Orientation accuracy
- < 1°
- Stabilization accuracy
- < 0,2°/s
- Telemetry and control
- UHF, S-band
- Operating temperature range
- -20...60 °C
3U
- Weight, w/o payload (w/ payload)
- 3 kg (5,5 kg)
- Lifetime
- Not less than 1 year
- Redundancy
- Partial (EPS)
- Average power available
- 10 – 15 W
- Average power requirement or on-board systems
- < 3 W
- Battery capacity
- ≈ 10 A × h
- Volume available for payload
- 2U (100 mm х 100 mm х 200 mm)
- On-board voltage and current load available for payload
- 3.3 V/5A; 5 V/3A; 8.4 V/2A
- Orientation accuracy
- < 1°
- Stabilization accuracy
- < 0,2°/s
- Telemetry and control
- UHF, S-band
- Operating temperature range
- -20...60 °C
6U
- Weight, w/o payload (w/ payload)
- 6 kg (8,5 kg)
- Lifetime
- Not less than 3 years
- Redundancy
- Hot redundant (OBC, EPS, ADCS)
- Average power available
- 12 – 20 W
- Average power requirement or on-board systems
- < 3 W
- Battery capacity
- ≈ 15 A × h
- Volume available for payload
- 5U (100 mm x 200 mm x 200 mm + 100 mm x 100 mm x 100 mm)
- On-board voltage and current load available for payload
- 3.3 V/5A; 5 V/3A; 8.4 V/2A
- Orientation accuracy
- < 1°
- Stabilization accuracy
- < 0,2°/s
- Telemetry and control
- UHF, S-band
- Operating temperature range
- -20...60 °C
12U
- Weight, w/o payload (w/ payload)
- 12 kg (16 kg)
- Lifetime
- Not less than 3 years
- Redundancy
- Hot redundant (OBC, EPS, ADCS)
- Average power available
- 30 – 50 W
- Average power requirement or on-board systems
- < 5 W
- Battery capacity
- ≈ 30 A × h
- Volume available for payload
- 10U (200 mm × 200 mm × 200 mm + 100 mm x 100 mm × 200 mm)
- On-board voltage and current load available for payload
- 3.3 V/5A; 5 V/3A; 8.4 V/2A
- Orientation accuracy
- < 1°
- Stabilization accuracy
- < 0,2°/s
- Telemetry and control
- UHF, S-band
- Operating temperature range
- -20...60 °C
What can we guarantee
Satellites based on the Cleon I platform
Norby
NORAD ID — 46494
- Estimated service life
- 3 years
- Weight
- 8.5 kg
- Orbit parameters
- Altitude — 1500 kmInclination — 82.5 degrees
- Dimensions
- 100 × 226.3 × 340.5 mm3
- Orientation Control Accuracy
- Roll — at least 1 degreePitch — at least 1 degreeYaw — at least 1 degree
Norby 2
NORAD ID — 57181
- Estimated service life
- 3 years
- Weight
- 8.5 kg
- Orbit parameters
- Altitude — 500-600 kmInclination — Sun Synchronous Orbit (SSO)
- Dimensions
- 100 × 226.3 × 340.5 mm3
- Orientation Control Accuracy
- Roll/pitch — at least 1 degreePropulsion System — noneOnboard data storage — 64 MbSpacecraft telemetry and commands, VHF band — 436.7 MHzPayload data, S-band — 2425 МHz