541 flight-proven satellite platforms, components and ground equipment from verified manufacturers worldwide.
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…
Consists of a flow regulator that regulates the total flow rate; anode and cathode restrictors that ensure the…
Consists of a flow regulator that regulates the total flow rate; anode and cathode restrictors that ensure the…
Consists of a flow regulator that regulates the total flow rate; anode and cathode restrictors that ensure the…
Consists of a flow regulator that regulates the total flow rate; anode and cathode restrictors that ensure the…
Consists of two xenon flow controllers. Propellant - xenon. Manufacturing lead time is given without taking into account…
Compact ADCS (1 deg pointing, 0.1 deg knowledge, CAN/USB/BT interfaces) for small spacecraft, 2 W average power.
Propellant - hydrazine. The main thruster component parts are: a decomposition chamber with a catalyst element and a…
Propellant - hydrazine. The main thruster component parts are: a decomposition chamber with a catalyst element and a…
Consists of two units: M-70 Stationary Plasma Thruster and Xenon Flow Controller Unit (XFC Unit). Propellant - xenon.…
Propellant - hydrazine. The unit consists of one modified thermocatalytic low thruster. Thermal mode of the unit is…
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