Space Hardware Marketplace

2368 flight-proven satellite platforms, components and ground equipment from verified manufacturers worldwide.

2368 products
Payloads & Instruments

GNSS-RO Atmospheric and Ionospheric Data

PlanetiQ
  • InstrumentPyxis GNSS-RO receiver (4th generation, NASA-heritage, rad-hard)
  • Signal sourcesGPS, GLONASS, Galileo, BeiDou
  • SNR1,500 V/V (60 dB-Hz) — 7.5× higher than competing instruments

High-resolution GNSS Radio Occultation data from LEO constellation delivering global atmospheric profiles at 100m vertical resolution with SNR…

Ground Segment

ELARA X-Band Multibeam Ground Antenna

Quasar Satellite Technologies
  • Frequency bandX-band
  • ArchitectureScalable, modular multibeam
  • ControlSoftware-Defined, dynamic configuration and automated tasking

Australian-designed scalable, software-defined X-band multibeam antenna for simultaneous multi-spacecraft tracking and communications, with commercial and defence dual-use capability.

Satellite Platforms

Puli Lunar Rover

Puli Space Technologies
  • 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.

Payloads & Instruments

Puli Lunar Water Snooper (PLWS)

Puli Space Technologies
  • 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…

Communications

QEYnet QKD Microsatellite Network

QEYnet
  • TechnologyQuantum key distribution (QKD) via free-space optical single-photon links
  • PlatformLEO microsatellites
  • Security basisLaws of quantum physics — unconditional security, not computational

Global LEO microsatellite quantum key distribution network providing unconditionally secure encryption key exchange impervious to quantum computing attacks.

Payloads & Instruments

Quub Earth Observation Constellation

Quub (Mini-Cubes)
  • 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.

Deployers & Separation Systems

Hyperion PocketQube Deployer

Quub (Mini-Cubes)
  • 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.

Payloads & Instruments

RCMOS Space Camera

Raptor Photonics
  • 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.

Payloads & Instruments

Ninox eSWIR 640 Space Camera

Raptor Photonics
  • Spectral rangeExtended SWIR (eSWIR), beyond 2 µm
  • Format640 pixels
  • ApplicationsHyperspectral imaging, night-time surveillance, thermal and mineral remote sensing

Extended-SWIR 640-pixel space camera for hyperspectral, thermal, and night-time remote sensing payloads on LEO CubeSats.

Payloads & Instruments

Eagle 47-10 Space Camera

Raptor Photonics
  • SensorBack-illuminated 1MP 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…

Satellite Platforms

RapidCube-20 CubeSat Bus

Rapid Cubes GmbH
  • CubeSat class20 kg
  • Size (stowed)22 x 22 x 44 cm (16U)
  • Bus architectureFailure-tolerant

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

Satellite Platforms

RapidCube-6 CubeSat Bus

Rapid Cubes GmbH
  • CubeSat class8 kg
  • Size (stowed)22 x 10 x 36 cm (6U) / 22 x 10 x 45 cm (6U XL)
  • Bus architectureFailure-tolerant

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

OBC & Avionics

RK410 High Reliability Space OCXO

Rakon Limited
  • Package size (LxWxH)99 x 88 x 54 mm
  • Nominal frequency5 to 10 MHz
  • Stability class10^-10

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

Payloads & Instruments

SpectraLoc Payload

Quadsat ApS
  • 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.

Test Equipment & EGSE

Quadsat Antenna Measurement System

Quadsat ApS
  • 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 & Navigation

ADCS control unit

SPUTNIX
  • Dimensions, mm101 x 100 x 20 (without fasteners)
  • Mass, g220
  • Power voltage, V6-36 (without galvanic isolation)

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

ADCS & Navigation

Reaction wheel

SPUTNIX
  • Dimensions, mm160 x 160 x 80 (without fasteners)
  • Mass, kg3.2
  • Power voltage, V22-34 (without galvanic isolation)

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