Complex IVK-M
Spacecraft comprehensive electrical test complex (334 discrete outputs, 324 inputs, 18 DC channels, 20-ch solar simulator, 27 V/5 A supply, QNX/Windows). Customizable.
Technical specifications
- Purpose
- Comprehensive spacecraft electrical testing and system verification
- Year of release
- 2019
- Guaranteed service life, years
- 10
- Estimated production/delivery time
- 12 months
- Customization
- Can be adapted to customer requirements
- Galvanic isolation
- Opto-relay
- Communication interfaces
- Ethernet, RS-232/422/485
- Discrete output signals
- 334
- Matrix commands
- 15×16 and 3×20
- Discrete input signals
- 324
- Dry matrix poll
- 16 words × 8 bits
- DC voltage measurement channels
- 18
- Temperature monitoring inputs
- 3 (1–50 °C)
- Insulation resistance monitoring channels
- 2 power lines
- Spacecraft supply voltage/current
- 27 V / 5 A
- Solar cell simulator
- 20 ch × 3.6 A + 10 ch × 3.0 A, Uxx ≤60 V
- Variable DC supply
- 24–37 V
- Variable DC current
- 0–7 A and 0–14 A, Uxx ≤60 V
- Software
- QNX, Windows, Microsoft Office, specialized test software
- UPS
- Yes
- TRL
- 9
About
The Complex IVK-M provides comprehensive ground-based electrical testing of spacecraft and verification of individual systems at manufacturers and operating organizations. It features galvanic isolation by opto-relay, universal Ethernet/RS-232/422/485 interfaces, 334 discrete output signals, 15×16 and 3×20 matrix commands, 324 discrete inputs, 16-word dry matrix poll, 18 DC voltage measurement channels, 3-input temperature monitoring (1–50 °C), telemetry processing, 2 power line insulation resistance channels. Power simulation: 27 V / 5 A spacecraft supply, 30-channel solar cell simulator (20 channels at 3.6 A, 10 at 3.0 A, Uxx ≤60 V), variable DC 24–37 V, programmable DC current (0–7 A and 0–14 A). UPS provided. Software: QNX, Windows, Microsoft Office. Released 2019, 10-year life, 12-month delivery. Customizable.
Documentation
No public datasheet yet — request the datasheet / ICD from the supplier.
