541 flight-proven satellite platforms, components and ground equipment from verified manufacturers worldwide.
Autonomous star tracker for GEO (0.8 kg, 5 W, 1.5 arcsec cross-boresight at 22 Hz) with 7+ years…
Autonomous star tracker for LEO up to 1200 km (0.5 kg, 5 W, 1.5 arcsec cross-boresight at 22…
Sun Sensor is a two orthogonal axes digital sun sensor. It generates the directional cosines of the angles…
Mechanical antenna reflector hold-down lock (600 kg clamping force, 200 N·m bending moment, 0.35 kg, 50-actuation life).
Mechanical antenna reflector hold-down lock (400 kg clamping force, 200 kg side load, 0.37 kg, 50-actuation life).
An upgraded version for KIND34-040. The small-size device for measuring the angular velocity is designed to measure the…
High-precision orientation and stabilization system for medium-orbit spacecraft with moments of inertia from 100 to 5000 kg·m². Made…
Raspberry Pi Compute Module nanosatellite OBC+ADCS carrier (60 g, CAN/I2C/SPI/UART, -40 to +60 °C) with integrated ADCS controller.
Flight-proven Raspberry Pi Compute Module nanosatellite OBC (59 g, CAN/I2C/SPI/UART) with sensor suite; flown on SiriusSat-1/2.
Flight-proven Raspberry Pi Compute Module sensor carrier board (55 g, CAN, 0.25 W) for nanosatellites; flown on SiriusSat-1/2.
Triple-core nanosatellite OBC (AVR + M0 + M4F, 200 MHz, 32 GB microSD, 9-DOF IMU, CAN/I2C/UART/SPI interfaces).
Flight-proven magnetic torquer assembly (6 × 1000 Am² rods, 50 kg, 50 W) for low-orbit spacecraft momentum unloading.
Dual-channel magnetic torquer driver board for nanosatellites, controlling external magnetic coils in solar panels (PWM, 3 W peak,…
Reaction wheels block contains four reaction wheels and provides work of three-axis orientation and stabilization system. Installation into…
Satellite laser ranging and velocity measurement system of spacecraft. It defines the distance considering the delay of reflected…
The small-size block for measuring the angular velocity is designed to measure the integrals of the absolute angular…
Redundant free form gyroscopic angular velocity vector meter for spacecraft orientation and stabilization control system. Sealed monoblock device,…
Redundant free form gyroscopic angular velocity vector meter for spacecraft orientation and stabilization control system. Sealed monoblock device,…
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