Satellite Platforms — Space Hardware Marketplace

Hyperfield-2

• Class / massMicrosatellite, 70 kg
• Spectral range450-1,650 nm
• Ground resolution15 m (hyperspectral)

70 kg hyperspectral microsatellite in development, extended spectral range and RGB camera, planned 2026 launch.

Hyperfield-1

• Class / mass6U CubeSat, 12 kg
• Orbit500 km polar sun-synchronous
• Spectral range475-950 nm

12 kg 6U hyperspectral CubeSat with a patented tunable VNIR imager, operational in orbit.

CubeSat Kit for Microchip PIC24 MCUs w/USB OTG

• MCUMicrochip PIC24FJ256GB210, low-power 16-bit, with USB OTG
• Processor modulePluggable Socketed Processor Module E (PSPM E) with PIC24FJ256GB210
• Processor module variantPluggable Processor Module E1 (PPM E1)

Pumpkin's complete CubeSat bus kit built around the Microchip PIC24FJ256GB210 low-power 16-bit MCU with USB On-The-Go support, bundling…

CubeSat Kit for Microchip dsPIC33 DSCs

• DSCMicrochip dsPIC33FJ256GB210, low-power 16-bit Digital Signal Controller
• Processor modulePluggable Socketed Processor Module D (PSPM D) with dsPIC33FJ256GP710
• Processor module variantPluggable Processor Module D2 (PPM D2)

Pumpkin's complete CubeSat bus kit built around the Microchip dsPIC33FJ256GB210 low-power 16-bit Digital Signal Controller, bundling structure, C&DH…

CubeSat Kit for Microchip PIC24 MCUs

• MCUMicrochip PIC24FJ256GA110, low-power 16-bit
• Processor modulePluggable Socketed Processor Module D (PSPM D) with PIC24FJ256GA110
• Processor module variantPluggable Processor Module D1 (PPM D1)

Pumpkin's complete CubeSat bus kit built around the Microchip PIC24FJ256GA110 low-power 16-bit MCU, bundling structure, command & data…

TY34 (SUSTech-1) Space Science Microsatellite

• Electric-field antenna lengthup to 12 m (world-record length for a microsatellite)
• Aurora observation duration9 minutes of continuous observation per polar pass
• PayloadsElectric-field measurement payload, aurora camera, Tiange gamma-ray burst detector, CXPD X-ray polarimeter, IP-based ground-link terminal, thermoelectric conversion verification unit

Microsatellite platform hosting a 12 m ultra-long electric-field antenna and aurora camera for magnetosphere and space-weather research.

TY-33 50kg-Class Satellite Platform

50kg-class scientific research satellite platform with high-precision thermal control, radiation-hardened composite structure, and long-duration power supply.

Honghu 50kg-Class Satellite Platform

50kg-class space science experiment satellite platform carrying integrated electronic and electric-propulsion payloads for in-orbit thruster verification.

Meridian Space LEO Satcom Constellation & Microsatellite Bus

Meridian Space's proliferated LEO satellite communications constellation, built on ~70 kg high-performance microsatellites, offering enterprise and government customers…

Satellite-as-a-Service (SataaS)

• Platform sizes offered6U, 12U
• Missions completed20 satellite missions in less than 5 years
• Flight cadence~4 flights per year

Shared 6U and 12U smallsat platforms with end-to-end launch, hosting, and data-delivery services for in-orbit demonstration and verification…

SSTL-MINI

• Payload massUp to 200 kg
• Payload peak powerUp to 2000 W
• Design life7 years

Customisable minisatellite platform built on strong flight heritage, supporting very high resolution imagers and SAR payloads.

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.

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.

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.

RapidCube-20 CubeSat Bus

• 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.

RapidCube-6 CubeSat Bus

• 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…

Satellite platform SXC12

A universal, combinable 12U CubeSat platform with flexible redundant subsystem configuration, high-speed X-band downlink, and gas propulsion system,…