Space Hardware Marketplace

Load-bearing Structure of the Enclosure. Type 6

• Angle between intersection nodes of spiral fins7.5°
• Angle between two spiral fins73°2'
• Spiral fins thickness6±0.5 mm

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

Modernized spherical glass satellite “BLITZ-M”

• PurposeProviding calibration of quantum-optical stations
• Year of release2013

The BLITZ-M is a spherical glass retroreflector satellite designed for calibrating quantum-optical stations.

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 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.