Space Hardware Marketplace

SSTL-MICRO

• Platform massFrom ~30 kg
• Payload massUp to 65 kg for payload chain
• Payload envelopeMax W 45 x L 34 x H 34 cm

Highly capable microsatellite platform offering strong payload power, mass capacity and redundancy.

SSTL-CUBE

• Form factor12U (Cube-Vista EO) / 8U (Cube-Signal comms)
• Payload compatibilityEarth imaging, software defined radio, small LEO telecoms, technology demonstration, radiation monitoring, AIS
• ProgrammeTraining Satellite Build Programme

Entry-level 12U cubesat platform designed for satellite build training missions.

Intelligent Space Systems Interface (iSSI)

Standard, robotic on-orbit connector/bus interface providing power, data, bandwidth and physical rigidity for modular payload integration.

Orbital Logistics Vehicle (OLV)

• Platform TypeModular satellite bus / space platform with common interface bus
• Core Interfaceintelligent Space Systems Interface (iSSI)
• iSSI FunctionStandard bus interface providing power, connectivity, bandwidth and physical rigidity (analogous to USB/PCI for satellites)

Modular space platform with open interface bus for hosting third-party payloads, assembled on-orbit at ISS.

Xovian RF Intelligence Satellite

• Signal domainFull-spectrum RF (radio frequency signals intelligence)
• CoveragePersistent, 24/7 global coverage across land, sea and air
• ArchitectureAI-native, vertically integrated from space to cloud

AI-native RF satellite for global signal intelligence and situational awareness.

Ka-Band Horn Antenna

• Frequency bandKa-band
• Antenna typeHorn antenna
• Beam characteristicHigh gain, directional

Miniaturized Ka-band horn antenna for small satellite ground communications, providing high-gain directional RF link in a compact package.

Ka-Band Datalink Transponder

• Frequency bandKa-band
• ApplicationHigh-rate satellite-to-ground datalink, Earth observation downlink
• Form factorCompact downlink transponder unit

Ka-band datalink transponder optimised for high-rate satellite-to-ground data downlink in LEO small satellite missions.

Ku-Band Transponder

• Frequency bandKu-band
• ApplicationEarth observation downlink, broadband, science missions
• Form factorCompact, miniaturized transponder

Compact Ku-band transponder for small satellite and CubeSat missions requiring high-throughput microwave communications links.

K/Ka-Band Transponder for 5G LEO

• Frequency bandsK-band (uplink) / Ka-band (downlink)
• Application5G NTN, LEO CubeSat and small satellite communications
• Form factorMiniaturized, integrated transponder

Miniaturized K/Ka-band transponder integrating uplink and downlink in a compact unit designed for 5G LEO CubeSat and small…

GNSS-RO Atmospheric and Ionospheric Data

• 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…

ELARA X-Band Multibeam Ground Antenna

• 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.

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…

QEYnet QKD Microsatellite Network

• 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.

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.