Conical Adapter. Type 2
GlavkosmosFlight-proven CFRP conical adapter (398.5 mm, 34 kg) interfacing spacecraft to the Fregat-SB upper stage on Zenit.
542 flight-proven satellite platforms, components and ground equipment from verified manufacturers worldwide.
Flight-proven CFRP conical adapter (398.5 mm, 34 kg) interfacing spacecraft to the Fregat-SB upper stage on Zenit.
Conical grid-shell adapter providing the mechanical interface between a spacecraft and its upper stage.
Conical grid-shell adapter providing the mechanical interface between a spacecraft and its upper stage.
Seven-reflector retroreflector array for precision laser ranging of the ESA Sentinel-3 spacecraft.
Interference-coated angle-reflector panel for laser ranging on the Luna-Globe lander/orbiter.
Compact four-reflector "Pyramid" retroreflector for onboard calibration on the Condor-FKA satellite.
36-reflector ring panel for metrological control and calibration of the GLONASS-K2 navigation constellation.
Charged particle detector was developed by Sputnix in collaboration with scientists from SINP (Moscow State Univercity). Detector provides…
ERS small-size multiband SAR, intended for operation aboard aircraft of different types. Mathematical, algorithmic and software.
Satellite multiband imaging system consist of two identical multispectral camera devices made in the form of separate structural…
On-board digital television system with up to 8 monoblock cameras and an onboard data recording/processing unit.
Ultra-black coatings with reflection of non-informational radiation in the spectral range of 0.42-2.5 microns no more than 0.5…
Infrared instrumentation for measuring the spectra of outgoing thermal radiation of the surface-atmosphere system with high spectral resolution…
Wide-angle 13-lens objective for detection of low-orbit space objects at altitudes from 120 to 500 km.
Long-focus lens objective (500 mm aperture, 4000 mm focal distance) for Earth remote sensing equipment.
Short-focus lens objectives (40 mm aperture, 40-200 mm focal distance) for Earth remote sensing payloads.
The On-board Memory Unit is designed to provide data storage for the remote sensing satellites payloads.
Asperical mirror Specific features: Item is produced in accordance with the Customer's working design documentation (WDD).
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