Space Hardware Marketplace

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 nanosatellite platform functional kit for studying satellite engineering principles, including design, assembly, testing…

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

A PC/104 compatible Payload Baseboard designed for the development of satellite payloads and other systems, featuring a microcontroller…

3U Cubesat Platform

The 3U Cubesat Platform is a universal satellite bus designed for operation in space conditions at altitudes up…

Conical Adapter. Type 1

The Conical Adapter Type 1 provides a specified interface between a spacecraft and an upper stage, featuring a…

Conical Adapter. Type 2

The Conical Adapter Type 2 is a flight-qualified CFRP conical grid shell designed to provide a specified interface…

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 the purpose of precision determination of spacecraft orbit parameters.
• Year of release2011

A retroreflector system designed for the Sentinel-3 spacecraft, consisting of seven angle reflectors with a double-spot directional pattern.

Retroreflector system for “Luna-Globe” spacecraft

• PurposeDesigned for re-reflection of laser radiation when measuring the range from ground quantum-optical stations to spacecraft.
• Year of release2013
• TypePanel of angle reflectors with interference coating of reflecting faces.

A retroreflector system designed for the Luna-Globe spacecraft, used for re-reflecting laser radiation to measure range from ground…

Retroreflector system “Pyramid” for “Condor-FKA” spacecraft

• PurposeRe-reflection of laser radiation in direction of quantum-optical station photodetector in order to calibrate on-board equipment.
• Year of release2016
• CompositionSmall-sized retroreflector system consisting of four angle reflectors

The "Pyramid" retroreflector system is a small-sized assembly of four angle reflectors designed for the 'Condor-FKA' spacecraft to…