Space Hardware Marketplace

TunaCan Thruster

Space-qualified, water-based electrothermal thruster that mounts externally in the 'tuna can' exclusion volume of CubeSat deployers, preserving 100%…

SOC-760 VNIR-SWIR Hyperspectral Imager

• Spectral regionsVNIR/SWIR
• Range400-2500 nm
• Spectral resolutionVNIR 2.5 nm / SWIR 5 nm

Portable dual-band (VNIR/SWIR) hyperspectral imager, 0.4-2.5 micron, 650 co-registered bands.

710 Series Hyperspectral Cameras (HyCore / OmniCore VNIR)

• Spectral range375-1025 nm
• Spectral channels784
• Spectral resolution (FWHM)1.65 nm

Compact VNIR hyperspectral camera family (375-1025 nm, 784 channels) with integrator and lab-tower configurations.

SOC-750 Midwave Infrared Hyperspectral Imager

• Spectral range2.0-5.0 micron
• Super frame rate11 datacubes/sec
• Frame size (standard)256x240 pixels

Real-time, military-grade MWIR hyperspectral imaging system for dynamic scenes, 2.0-5.0 micron.

410-DHR Reflectometer

• Measured quantityDirectional-hemispherical reflectance (DHR)
• OutputAbsolute reflectance (0-1) plus calculated in-band emissivity
• Spectral bands0.9-1.1, 1.9-2.6, 3.0-4.0, 3.0-5.0, 4.0-5.0, 8.0-12.0 micron

Portable handheld directional-hemispherical infrared reflectometer, developed with NAVAIR/NRL/NIST, 0.9-12 micron, two incidence angles.

SOC-210 Bidirectional Reflectometer

• Spectral range0.35-14 micron
• Incident polar angle0-85 degrees
• Incident azimuth angle0-360 degrees

Automated goniometric instrument measuring BRDF/BTDF over 0.35-14 micron with full hemispherical angular coverage.

SOC-100 Hemispherical Directional Reflectometer

• Spectral range2.0-25.0 micron (5000-400 cm-1)
• MethodAutomated reflectometer with 18-inch electroformed hemiellipsoid
• CalibrationComparison scans vs. calibrated specular gold standard

FTIR-attachment reflectometer measuring polarized, angular diffuse reflectance from 8 to 80 degrees incidence across 2.0-25.0 micron.

Satellite Platform SXC12

• Form factor12U
• Orbit altitudeUp to 600 km (LEO)
• Active life1.5-3 years

12U satellite bus for LEO missions up to 600 km altitude with 1.5-3 year active life and gas…

Satellite Platform SXC6 ADC (SXC6-ADC)

• Form factor6U
• ADCS3-axis
• Payload volume4U

6U CubeSat bus with 3-axis ADCS configuration and 4U payload volume.

OrbiCraft-Pro 3U Experimental (SXC3)

• Solar panelsSilicon
• Form factor3U

3U CubeSat platform with silicon solar panels for educational and technology-demonstration use.

Satellite Platform SXC6 RS (OrbiCraft-Pro 6U)

• Form factor6U
• ADCS pointing accuracy0.1 degree
• X-band downlinkDVB-S2, 10 Mbit/s

Full 6U CubeSat bus with star tracker, redundant systems, and X-band downlink, flight-proven on the OrbiCraft-Zorkiy Earth-observation mission.

Satellite Platform SXC6 Basic (SXC6-VOL)

• Form factor6U
• Max payload volume5U

Minimal-configuration 6U CubeSat bus maximizing payload volume up to 5U.

OrbiCraft-Pro 3U Profi (SXC3-GA-ADC)

• ADCS3-axis, reaction wheels + 5 sun sensors
• Solar panelsGaAs

3U CubeSat platform with 3-axis ADCS, reaction wheels, and 5 sun sensors for precision pointing missions.

OrbiCraft-Pro 1U Experimental (SXC1)

• Mass0.9-0.95 kg
• Dimensions108 x 108 x 113.5 mm
• Battery capacity39 Wh

1U CubeSat platform kit with silicon solar panels for educational and laboratory use.

OrbiCraft-Pro 1U Flight (SXC1-GA)

• Mass (with payload)1.33 kg
• Solar panelsGaAs
• ADCSElectromagnetic, B-dot detumbling control

Flight-ready 1U CubeSat platform with GaAs solar panels and electromagnetic ADCS.

OrbiCraft-Pro 3U Flight (SXC3-GA)

• Mass1.45 kg (4 kg max with payload)
• Solar panels14, GaAs

Flight-ready 3U CubeSat platform with GaAs solar panels across 14 panel faces.

ThinkX

• CapabilityInterior imaging of target object (material characterization / threat assessment)
• RangeProximity and long-distance imaging up to 10 km
• ApplicationSpace domain awareness, counterspace operations

Space-based space domain awareness (SDA) autonomous platform-to-platform X-ray imaging system.

ThinkToolkit

• Welding methodElectron beam welding
• Weld capacity30 cm of steel in a single pass
• Energy efficiency> 90%

Robotic arm and arm-agnostic end-effector suite for in-space servicing, construction, and inspection, including flight-proven electron-beam welding.