Space Hardware Marketplace

Supernova

• PropulsionSolar Thermal Propulsion (STP) with deployable mirror concentrators
• Delta-v~6 km/s
• TaskabilityOn-standby, taskable in minutes

Maneuverable, solar-thermal-propulsion spacecraft delivering ~6 km/s of delta-v with on-demand taskability from LEO to cislunar space.

Puli Lunar Rover

• Design philosophyLightweight, low-cost planetary rover
• Terrain capabilityUnique mobility on rough lunar and planetary surfaces
• Payload compatibilityConfigured to carry PLWS neutron spectrometer and other scientific payloads

Lightweight, low-cost planetary rover with unique mobility capabilities for lunar surface operations and payload delivery in rough terrains.

Puli Lunar Water Snooper (PLWS)

• Instrument typeMiniature neutron spectrometer
• MeasurementAlbedo neutron count rates (subsurface hydrogen / water ice proxy)
• Mission heritageIM-2 (Intuitive Machines), launched February 2025, Micro Nova Hopper

NASA-prize-winning miniature neutron spectrometer for mapping water ice in lunar south polar soil, flight-proven on Intuitive Machines' IM-2…

Quub Earth Observation Constellation

• PlatformPocketQube-class microsatellites
• ApplicationsWater resources, forests, crops, air quality monitoring
• Ground systemsAI-powered imagery processing

PocketQube constellation delivering high-frequency Earth observation imagery for water, agriculture, disaster response, and air quality monitoring.

Hyperion PocketQube Deployer

• Compatible formats1P through 6P PocketQube
• ApplicationsTechnology demonstration, scientific payloads, commercial constellations, educational missions
• InterfacesStandardized PocketQube interfaces

Flight-ready PocketQube deployment system supporting 1P–6P missions for launch providers and satellite developers seeking affordable orbit access.

RCMOS Space Camera

• Sensor typeCMOS, global shutter, progressive scan
• Spectral range0.3–1.1 µm (visible + NIR)
• VariantsMono and colour

Space-qualified CMOS camera for LEO CubeSat integration, combining compact form factor with high sensitivity across 0.3–1.1 µm.

Raptor Photonics Space Camera Solutions

Raptor Photonics offers flight-ready COTS and custom OEM camera solutions for LEO CubeSat missions, covering UV to SWIR…

Eagle 47-10 Space Camera

• SensorBack-illuminated 1 MP CCD (Teledyne e2v)
• Pixel size13 µm x 13 µm
• Peak qe>90% @ 525 nm; 50% @ 380 nm and 720 nm

Deep-cooled back-illuminated 1MP CCD space camera with 7-year vacuum guarantee and >90% QE at 525 nm for LEO…

RapidCube-20 CubeSat Bus

16U, 20 kg CubeSat bus with failure-tolerant architecture supporting 5–10 kg payloads, S/X-band links, and SSO IOD/IOV missions.

RapidCube-6 CubeSat Bus

6U CubeSat bus platform with failure-tolerant architecture, S/X-band links, and configurable attitude control for LEO missions up to…

RK410 High Reliability Space OCXO

MIL/ECSS-qualified space oscillator with 10^-10 stability class, used operationally by international space agencies for decades.

SpectraLoc Payload

• CapabilitiesPassive emitter detection, classification, direction-finding, geolocation
• Detection rangeExtended line-of-sight
• Platform compatibilityFixed-wing drones, quadcopters, VTOL platforms (small UAVs)

Compact airborne RF payload for passive threat detection, direction-finding, and geolocation, built for small UAV integration.

Quadsat Antenna Measurement System

• Measurement capabilitiesPointing accuracy, tracking and handover, radiation pattern raster and cut, cross-polar discrimination, gain, EIRP, G/T
• Antenna types supportedMulti-beam, flat-panel, electronically steerable (LEO and multi-orbit)
• Lifecycle coverageManufacturing QC, vendor type approval, factory/site acceptance testing, in-situ deployment calibration, ongoing performance monitoring

Drone-based satellite antenna test and calibration system supporting the full antenna lifecycle, tailored for LEO and multi-orbit terminals.

ADCS control unit

A dual-redundant attitude control and stabilization system control unit (OSSCU, SX-SBOX-ADCU-01) running SPUTNIX's flight-qualified ADCS software.

Reaction wheel

A control flywheel motor (CFM, SX-SBOX-RWH-50-2.0-01) generating control torque via rotor acceleration/deceleration for larger satellite platforms.

Magnetic torquers

A family of proprietary magnetic torquer rods (SX-MT-1 through SX-MT-30) used with the magnetic torquers control unit for…

Magnetic torquers control unit

A control unit (SX-SBOX-MTQU-01) driving up to three magnetic torquers via PDM channels to implement angular velocity damping…

Magnetometer

A triaxial anisotropic-magnetoresistive magnetometer (SX-SBOX-MAG-01) used in attitude determination alongside magnetic torquers for detumbling and momentum unloading.