539 satellite platforms, components and ground equipment from manufacturers worldwide.
A programmable real-time control complex for monitoring the shape and dimensional deviations of large-sized product forms (10 m…
An angular accelerometer designed for integration into gyro-stabilized platforms, providing measurement of apparent acceleration for ballistic and space…
A string accelerometer designed to measure the apparent acceleration of space objects, with flight heritage on the Soyuz…
A bipropellant thruster designed for the Briz-M booster, providing attitude control for spacecraft using UDMH/NTO propellants.
The Fregat Universal Upper Stage is designed to serve as the third stage of launch vehicles, enabling the…
The Dynamic Pressure Sensor Vt 206 is a strain gauge sensor designed for measuring static-dynamic pressure in liquid…
The Pressure Sensor DAV 067 converts absolute pressure of liquid and gaseous aggressive and non-aggressive working media into…
The DAV 068 is a flight-qualified pressure sensor designed for measuring absolute pressure of liquid and gaseous media…
The Transition Compartment is a structural component for launch vehicles, designed to ensure the docking of the space…
A two-phase asynchronous controlled electric motor with a hollow non-winding rotor, designed for automation systems requiring low-power drive…
The Thermoelectric Converter DT 27 is a flight-qualified sensor designed for temperature measurement of aggressive (liquid oxygen) and…
The DHS 514 Pressure Converter is a piezoelectric transducer designed to measure acoustic pressures of non-aggressive gaseous media…
The DHS 517 Pressure Converter is a flight-qualified piezoelectric transducer designed to measure sound pressure of non-aggressive gaseous…
The Fairing is a head fairing designed to protect spacecraft and upper stages from aerodynamic and thermal loads…
The DRI 095 is a flight-qualified differential pressure sensor designed for monitoring and control systems in rocket and…
Flight-proven strain-gauge absolute pressure sensor (0–11 kPa, 5% error, 0.35 kg) for liquid rocket engine control and diagnostics.
The RD-171 M is a powerful liquid rocket engine designed for the first stage of the Zenit launch…
The RD-180 is a liquid rocket engine with afterburning of oxidizing gas, designed for the first stage of…
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