Space Hardware Marketplace

SKY-I

• Data sourcesProprietary Data DOTS sensors plus external environmental data sources
• AccessAPI access, demo booking
• ModulesSkyLens, SkyBlueprint, SkyWard

Space environmental intelligence platform fusing proprietary in-orbit sensor data with external sources for mission planning and operations.

Data DOTS

• Measured parametersRadiation levels, electromagnetic interference
• FunctionIn-orbit environmental sensing, data relay to SKY-I platform
• Flight heritageFirst unit launched January 2025 as hosted payload on D-Orbit ION Satellite Carrier, sun-synchronous LEO

Compact, intelligent in-orbit sensing payloads measuring radiation and electromagnetic interference to feed the SKY-I platform.

SC-OBC Module A1

CubeSat onboard computer built on a Xilinx Artix-7 FPGA running Zephyr RTOS.

SpaceBolt

• EvaluationPositively evaluated by ESA in a 6-month process
• Data importNASTRAN .PCH files, plain CSV, statics/sine/random loads
• ProcessingThousands of load cases processed in seconds

Software for verifying thousands of bolted joints under space environments, ESA-evaluated.

SpaceVibe

• Supported file formatsNastran punch (PCH), universal 58 (UNV), CSV
• StandardsECSS-E-HB-32-26, NASA-HDBK-7004
• Comparison levelsQSL, sine, PSD, RRS

Vibration test data processing and visualization tool for faster, safer spacecraft vibration testing.

Precision Assemblies

• In-house processesBolting, riveting, bonding, alignment, measurement
• Satellite/launcher structuresPrimary/secondary structures, integrated radiator functionalities, launch vehicle adapters
• Manned space applicationsISS, Orion, Lunar Gateway — fracture control and human-factors design

High-performance satellite and launcher structures, optical payload structures, and electronic equipment structures built to spec in-house.

Honeycomb Sandwich Panels

• Facesheet/core combinationsAluminium/aluminium, GFRP/aluminium, CFRP/aluminium, CFRP/CFRP; NOMEX cores optional
• Insert materialsAluminium, titanium, INVAR, CFRP
• Insert typesFloating, face-to-face, edge, block

Custom honeycomb sandwich panels in aluminium, GFRP and CFRP face-skin/core combinations for satellite and launcher structures.

SpaceStrut Struts and Booms

• Hybrid Strut constructionComposite tube (filament winding, thermoplastic, or prepreg) with metallic fittings (aluminium, titanium, invar, others)
• Full CFRP Strut constructionIntegral single CFRP piece with continuous fibres including fittings
• DoubleZero variantZero coefficient of thermal expansion and zero moisture expansion

Family of lightweight, high-stiffness structural parts including struts, booms, rods, bars and beams with low thermal expansion.

TangoBox

• RoboticsIntegrated six-axis robotic arm plus traditional automation
• Supported subsystemsSpectroscopy, centrifuges, incubators, microplate readers, DNA analyzers, single-cell genetic sequencers
• Manufacturing standardGood Manufacturing Practices (GMP)

Modular, automated in-space laboratory and manufacturing facility with integrated robotics for pilot-scale and commercial on-orbit manufacturing.

CubeLabs

• Base form factor9U (scales beyond 9U)
• Thermal control minimum temperature4 degrees C
• Onboard automationBuilt-in flight computers for automated control and near-real-time data relay

Standardized, modular automated hardware platform for R&D and manufacturing investigations aboard the ISS.

UNIKA HDRM Preload Device

• Mechanical interfaceUser customized mating head
• Release bolt threadUser customized up to M10
• Generated preloadUp to 50 kN @ max 3 mm travel

Compact, electronically-controlled 50 kN preload/tensioning device for Hold Down and Release Mechanisms, cleanroom-safe.

ATLAS ICU (Initiation Control Unit)

• Actuation stepsActivation, arming, fire
• Power source50 A / 12 V / 600 W
• Number of actuatorsUp to 5 actuators (10 power lines)

PC-controlled current-pulse generator and control electronics for synchronized initiation of release actuators in ground testing.

ATLAS22 Ground Test Release Actuator

• Mechanical interfaceUser customizable (to match NEA, Glenair, Eaton, Arquimea)
• Release bolt threadUser customizable up to M8
• Max. release preload22 kN

Rapidly resettable, non-explosive hold-down and release actuator for ground testing and qualification of space mechanisms.

Ultraprecision Machining and Polishing Services

• CNC machining5-axis, parts up to 650 mm
• Ultraprecision machiningDiamond turning, milling and ruling, up to 500 mm
• PolishingMRF and computer-controlled polishing, up to 1 m, surface roughness < 0.2 nm rms

5-axis CNC machining, diamond turning, and computer-controlled polishing services for precision optical and mechanical parts up to 650…

Mirror Systems and Opto-Mechanical Assemblies

• System typesTelescope optics, spectrometer optics, illumination/beam-shaping optics, athermal systems
• Opto-mechanical assembliesTelescope structures, optical frames, flexures, hinges, ground support equipment

Complete mirror systems and opto-mechanical assemblies for telescopes, spectrometers, and beam-shaping optics.

Custom Metal Optical Mirrors

• Mirror typesFlat, spherical, aspherical, freeform
• MaterialsAluminum, AlSi, gold, copper, NiP, crystals, polymers
• Standard diameterUp to 600 mm (larger on request)

Flat, spherical, aspherical, and freeform mirrors machined directly from metal for space and scientific optical systems.

Amun

• Operating temperature-40 C to +85 C
• Dimensions95.9 x 90.2 x 19.7 mm (0.2U)
• Mass185 g

PC/104 form-factor power management unit for 0.5U-2U CubeSats.

Ra

• Operating temperature-40 C to +125 C
• Efficiency> 30%
• Configurations1U / 2U / 3U / 6U / 8U plus custom design

High-efficiency, customizable solar panels for nanosatellites, offered in 1U-8U and custom configurations.