215 flight-proven satellite platforms, components and ground equipment from verified manufacturers worldwide.
Two-degree-of-freedom electromechanical device for transferring the reflector boom from the transportation to the operational position and for antenna…
Shock-free electromechanical release device (6 kg rod load, 0.08 kg, 41×41.5×41 mm, 75 actuations, flight-proven 2019).
Shock-free electromechanical release device (4 kg rod load, 0.05 kg, Ø38×41.7 mm, 50 actuations, flight-proven 2019–2020).
Linear electromechanical mast for umbrella-type reflector deployment (12 kg, 4100 mm length, 0.1 mm precision, 50 cycles).
2-DOF electromechanical antenna pointing drive (±25° per axis, 30 N·m, 3 kg·m² load inertia, 10-year life).
2-DOF electromechanical antenna pointing drive (±10°/±90° per axis, 60 N·m, 15-year life) for GEO missions.
Two-degree-of-freedom electromechanical drive for antenna pointing. Operating regimes: tracking, pointing.
1-DOF electromechanical thruster pointing drive (±10.5°, 20 N·m, 7.3 kg, 520×390×300 mm) with 15-year life. Flight proven.
Flight-proven pyrotechnic hold-down and separation lock (8500 kg clamping, 0.37 kg, 2 A actuation) with Glonass heritage.
Two-degree-of-freedom electromechanical device for transferring the reflector boom from the transportation to the operational position and for antenna…
Electromechanical device based on linear drives, which is designed to adjust reflective surface profile of the large reflector.
High-precision harmonic drive for antenna pointing (Ø85 × 23.5 mm, ±40 arcsec transfer error, 200,000 rev life, 15-year…
High-precision harmonic drive for antenna pointing (Ø85 × 34 mm, ±30 arcsec transfer error, 200,000 rev life, 15-year…
High precision electromechanical drive of linear positioning. 2 commutator electric motors (1 is in reserve).
Device for manual start-up of pico and nanosatellites from International Space Station (ISS). Supplied with remote control. There…
Electromechanical hold-down and release device (1000 kg clamping force, 0.455 kg, 50 actuations, 3–8 A actuation current).
2-DOF electromechanical antenna pointing drive (±25° per axis, 65 N·m, 150 kg·m² load inertia, 10-year life).
Mechanical antenna reflector hold-down lock (600 kg clamping force, 200 N·m bending moment, 0.35 kg, 50-actuation life).
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