Platform Components:
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Structural frame;
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PC/104-format subsystem boards;
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Optical sensors;
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GLONASS/GPS receiver;
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Solar panels;
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On-board auxiliary radio system;
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Payload adapter.
Application Scenarios:
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D33 small spacecraft;
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Relay satellite;
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Performing experiments in open space.
UKP3 Three-Axis Attitude Control System:
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Optical sensors;
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Magnetometer;
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Angular rate sensors;
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GLONASS/GPS receiver;
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Reaction wheels and magnetorquers (for attitude control).
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VHF band transceiver;
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Deployable antennas.
Technical Specifications
| Platform Mass | 3.2 kg |
| Dimensions (Transport State, L×W×H) | 120×120×378 mm |
| Dimensions (Operational State, L×W×H) | 765×765×378 mm |
| Minimum Battery Capacity | 48 Wh |
| Attitude Control System Type | Three-axis |
| Slew Rate | Up to 4 °/s |
| Axis Pointing Accuracy | ≤ 3° |
| Auxiliary Radio Link Frequency | 150 MHz, 430 MHz |
| Maximum Payload Dimensions (L×W×H) | 95×95×120 mm |
| Payload Interface | CAN, UART |
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