449 satellite platforms, components and ground equipment from manufacturers worldwide.
A three-channel fiber-optic gyroscope sensor designed to measure angular velocity vector projections and transmit this data to a…
A redundant, free-form gyroscopic angular velocity vector meter designed for spacecraft orientation and stabilization control systems, featuring four…
An Inertial Measurement Unit (IMU) designed for future manned spacecraft, providing precise measurement of velocity and angle increments…
The Kinetic Moment Reset System 1207 is designed to calm low-orbit spacecraft and dissipate accumulated kinetic moment from…
The Backup Inertial Measuring Device is a sealed monoblock unit designed to measure angular velocities in three axes,…
The Electromagnet EM-IF-20 is a core electromagnet designed for the stabilization equipment of spacecraft, featuring a harness and…
The Electromagnetic Unit (EMU) is a magnetic torquer for nanosatellites, designed to create a dipole magnetic moment proportional…
The Electromagnetic Unit (EMU) is a magnetic torquer designed for spacecraft attitude control systems, creating a dipole magnetic…
An Altitude Control System (ACS) designed for spacecraft, providing orientation accuracy of 1 degree and stabilization accuracy of…
Attitude-control actuators of the SX-SBOX suite for microsatellite platforms: ADCS control unit, reaction wheel, magnetorquers and a magnetorquer…
Attitude-determination and navigation sensors of the SX-SBOX suite for microsatellite platforms: satellite navigation, GNSS antenna, MEMS and fiber-optic…
Air table for testing relative motion of spacecraft: a precision aluminium horizontal surface with an even grid of…
Bench for calibration and verification of small matrix and diode-type sun sensors (linear and two-dimensional). The sensor is…
Hardware-in-the-loop simulation bench for developing and verifying attitude determination, stabilization and navigation systems of small spacecraft under conditions…
Sun sensor for nanosatellite attitude determination and control. The CAN interface allows a single sensor or a daisy-chain…
4-flywheel reaction wheel module for 3U+ CubeSats. DC brushless motors with vacuum-rated bearings, CAN interface per driver, ±5000…
Momentum reaction wheels for CubeSat attitude control — single unit (RW0) or 4-wheel cluster (4RW0).
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