Complex IVK-SOK-M
- Purpose: Designed for testing the spacecraft orientation system.
- Year of release: 2009
- Guaranteed service life (years): 10
- Estimated production / delivery time (months): 12
- Possibility to adapt the product to customer requirements: Да
| Parameter | Value |
|---|---|
| Universal Communication Interfaces | MIL-STD-1553B |
| Programmable DC voltage supply with periodic voltage value monitoring | (24 - 31) V, up to 3.5 A, 3 channels |
| Formation of a long management team | U ≤ 15 V, (0.5 - 1.5) A, load (6 - 8) Ohm |
| On-off signal generation | (90 ± 5) mA, (12 ± 2) mA, 11 channels |
| Analog Signal Conditioning | ± 10 V, ≤ 5 mA, 6 channels |
| Control of parameters of on-off signals | (24 - 31) V, 0.2 A, (0.03 - 10) s, 6 channels |
| Control of on-off signals of the | ≤ 15 V, ≤ 5mA, 42 channels |
| Monitoring the condition of temperature sensors (external device) | Rх = (50 - 100) Ohm, 8 channels |
| Simulation and compensation of the Earth's magnetic field | ±10 V |
| Reception and processing of packet pulse telemetry via a serial channel: packet size, packet repetition rate, pulse repetition rate | 512 bit, 50 Hz, 40 kHz |
| Reception and processing of parallel code | 12 bits, frequency 40 Hz |
| Uninterruptible power supply for the correct completion of the test program in the event of a power failure | Yes |
| Software | Windows OS, special software for preparing and executing test programs, test software |
- IVK-SOK-M contains an industrial computer, a device for interfacing a computer with a spacecraft orientation system, a cross, a product simulator.
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