Structures & Mechanisms — Space Hardware Marketplace

Antenna Reflector Hold-down Lock (mechanical) Type 2

Mechanical antenna reflector hold-down lock (400 kg clamping force, 200 kg side load, 0.37 kg, 50-actuation life).

Load-bearing Structure of the Enclosure. Type 5

• Angle between intersection nodes of spiral fins7.5°
• Angle between two spiral fins59.5°
• 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 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.

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.

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.

SX-SBOX Thermal Control (Microsatellite)

Thermal-control line of the SX-SBOX suite for microsatellite platforms: the thermal-control-system control unit (BU-SOTR) and engineering services for…

16U CubeSat Structure

Robust, modular 16U CubeSat structure with flight-proven heritage. Lightweight aluminum frame with hard-anodized finish, designed for seamless assembly…

12U XL CubeSat Structure

Robust aluminum 12U XL frame for advanced CubeSat and SmallSat missions. Modular design enables vertical and horizontal assembly…

EXOtube

Launch vehicle-agnostic universal modular adapter for rideshare missions, accommodating CubeSats to 1000 kg microsatellites.

EXOport

• Interface ports15" or 24" ESPA / SpaceX Dispenser Ring
• Compatible separatorsCarboNIX 8", 15", 18.25", 24"
• Compatible deployersEXOpod Nova, EXOpod AIR

Multi-satellite adapter mounting a full smallsat cluster on a single 15" or 24" ESPA/SpaceX Dispenser Ring port; 8…

Electric Lock 28V

28V electromechanical lock for triggering rocket/space hardware actuators.