Space Hardware Marketplace

Nanosatellite Engineering Model SamSat-A

• ContainsNanosatellite laboratory model, suspension system, debugging module, software
• Attitude control systemUniaxial
• Attitude control system componentsMagnetic coils, reaction wheel

Ground-based nanosatellite engineering model for developing and testing scientific payloads, software and onboard systems.

Nanosatellite Platform of CubeSat 3U Format

SamSat 3U CubeSat platform for scientific and technological experiments, with ~2 dm³ of payload volume.

Nanosatellite Platform

Modular nanosatellite bus for spacecraft separation control, in-orbit monitoring, Earth remote sensing and space-debris/precursor detection missions.

“OrbiCraft 3D” nanosatellite functional kit

OrbiCraft 3D is an educational kit for nanosatellite platform design. The kit is delivered in a basic configuration…

Conical Adapter. Type 5

Conical grid-shell adapter providing the mechanical interface between a spacecraft and its upper stage.

Load-bearing Structure of the Enclosure. Type 1-A

• Angle between intersection nodes of spiral fins6°
• Angle between two spiral fins28°
• Spiral fins thickness6+1 mm

Cylindrical CFRP grid-shell load-bearing structure for mounting spacecraft subsystems and equipment.

Load-bearing Structure of the Enclosure. Type 1-B

• Angle between intersection nodes of spiral fins6°
• Angle between two spiral fins28°
• Spiral fins thickness6+1 mm

Cylindrical CFRP grid-shell load-bearing structure for mounting spacecraft subsystems and equipment.

Load-bearing Structure of the Enclosure. Type 2

• Angle between intersection nodes of spiral fins7.5°
• Angle between two spiral fins42°
• Spiral fins thickness10±1 mm

Cylindrical CFRP grid-shell load-bearing structure for mounting spacecraft subsystems and equipment.

Load-bearing Structure of the Enclosure. Type 3

• Angle between intersection nodes of spiral fins7.5°
• Angle between two spiral fins58.9°
• Spiral fins thickness3±1 mm

Cylindrical CFRP grid-shell load-bearing structure for mounting spacecraft subsystems and equipment.

Load-bearing Structure of the Enclosure. Type 4

• Angle between intersection nodes of spiral fins7.5°
• Angle between two spiral fins42°
• Spiral fins thickness4.5±1 mm

Cylindrical CFRP grid-shell load-bearing structure for mounting spacecraft subsystems and equipment.

Payload Baseboard

The vacant area of the board is 2.54mm pitch breadboard where user can place any needed components to…

3U Cubesat Platform

Universal 3U CubeSat bus rated to 1500 km altitude, 3 kg dry mass, 2U/2.5 kg payload accommodation.

Conical Adapter. Type 1

Flight-proven CFRP conical adapter (650 mm) interfacing spacecraft to the Briz-M upper stage on Proton.

Conical Adapter. Type 2

Flight-proven CFRP conical adapter (398.5 mm, 34 kg) interfacing spacecraft to the Fregat-SB upper stage on Zenit.

Conical Adapter. Type 3

Conical grid-shell adapter providing the mechanical interface between a spacecraft and its upper stage.

Conical Adapter. Type 4

Conical grid-shell adapter providing the mechanical interface between a spacecraft and its upper stage.

Retroreflector system for AC (spacecraft) Sentinel-3 (ESA)

• PurposeReflection of quantum-optical station radiation for precision spacecraft orbit determination
• Year of release2011
• HeritageFlown on ESA Sentinel-3 spacecraft

Seven-reflector retroreflector array for precision laser ranging of the ESA Sentinel-3 spacecraft.

Retroreflector system for “Luna-Globe” spacecraft

• PurposeRe-reflection of laser radiation for ground-to-spacecraft ranging
• Year of release2013
• HeritageDeveloped for Luna-Globe lunar mission

Interference-coated angle-reflector panel for laser ranging on the Luna-Globe lander/orbiter.