Complex IVK-SOK-M
Spacecraft orientation system test complex (MIL-STD-1553B, magnetic field simulator, 42-ch signal monitoring, UPS, Windows) for ADCS testing. Customizable.
Technical specifications
- Purpose
- Spacecraft orientation system (ADCS) testing
- Year of release
- 2009
- Guaranteed service life, years
- 10
- Estimated production/delivery time
- 12 months
- Customization
- Can be adapted to customer requirements
- Communication interface
- MIL-STD-1553B
- DC voltage supply
- 24–31 V, up to 3.5 A, 3 channels (programmable)
- On-off signal generation
- 90±5 mA / 12±2 mA, 11 channels
- Analog signal conditioning
- ±10 V, ≤5 mA, 6 channels
- On-off signal monitoring channels
- 42 (≤15 V, ≤5 mA)
- Temperature sensor monitoring
- 8 channels, Rx=50–100 Ω
- Magnetic field simulation/compensation
- ±10 V
- Telemetry
- 512-bit packet, 50 Hz rate, 40 kHz pulse rate
- Parallel code input
- 12 bits, 40 Hz
- Software
- Windows OS, specialized test software
- UPS
- Yes
- TRL
- 9
About
The Complex IVK-SOK-M is designed for testing spacecraft orientation systems (ADCS). It uses MIL-STD-1553B interface and includes: programmable 3-channel DC voltage supply (24–31 V, up to 3.5 A), 11-channel on-off signal generation (90±5 mA and 12±2 mA), 6-channel analog signal conditioning (±10 V, ≤5 mA), 6-channel on-off signal parameter control, 42-channel on-off signal monitoring (≤15 V, ≤5 mA), 8-channel temperature sensor monitoring (Rx=50–100 Ω), Earth magnetic field simulation and compensation (±10 V), packet pulse telemetry (512-bit packets, 50 Hz, 40 kHz), 12-bit parallel code input (40 Hz), UPS. Software: Windows OS with specialized test programs. Contains industrial computer, spacecraft interfacing device, cross-switch, and product simulator. Released 2009, 10-year life, 12-month delivery. Customizable.
Documentation
No public datasheet yet — request the datasheet / ICD from the supplier.
