447 flight-proven satellite platforms, components and ground equipment from verified manufacturers worldwide.
Sun Sensor is a two orthogonal axes digital sun sensor. It generates the directional cosines of the angles…
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…
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,…
Monoblock device includes electronic and optoelectronic modules and a block of sensitive elements containing three mutually orthogonal sensitive…
Redundant free form gyroscopic angular velocity vector meter for spacecraft orientation and stabilization control system. An unsealed two-block…
Sealed monoblock device including electronic and opto-electronic modules with a block of sensitive elements, containing three mutually orthogonal…
Kinetic moment reset system. Structurally, the product consists of: - 2 primary converters of the geomagnetic field PGP-3M,…
Compact sealed fiber-optic gyro IMU (3-axis angular rate) being developed for future manned spacecraft, 10-year service life.
The core electromagnet for the stabilization equipment of the spacecraft with a harness on which the connector is…
Electromagnetic unit (EMU) - Magnetic Torquer for nanosatellites. There is an option to develop and supply EMU with…
Electromagnetic unit (EMU) - Magnetic Torquer There is an option to develop and supply EMU with magnetic moment…
We use cookies. Strictly necessary cookies keep the platform working. With your consent we also use Google Analytics to understand how the platform is used and improve it. We do not use advertising cookies. Cookie Policy · Privacy
Favorites are available to clients only. Sign in to your client cabinet or create a free account — it takes less than a minute.
How is your experience with the platform? Your message goes straight to our team.
Thank you! Your feedback has been sent to our team.
