Space Hardware Marketplace

Nereus 20 M

Monopropellant in-space thruster (5-22 N) running on green, storable hydrogen peroxide (H2O2) for satellite station-keeping, attitude control and…

AgriBlinkR

Low-power satellite-linked smart sensor for connected agriculture, delivering environmental updates from fields, reservoirs, and irrigation systems.

BlinkSat Radio

Low-power satellite receiver payload mounted on Blink Astro's PanelSat nanosatellites, capturing brief IoT sensor transmissions from the ground.

PanelSat

• MassApprox. 2 kg
• Length and Width22 cm x 22 cm
• Thickness3.5 cm

Blink Astro's compact nanosatellite platform hosting the BlinkSat Radio payload, forming the space-based backbone of its low-power IoT…

AquaBlinkR

• Frequency1616 - 1626.5 MHz
• Sensitivity-116 dBm
• Max EIRP29.8 dBm

Rugged low-power satellite-linked sensor for long-term waterway monitoring, reporting GPS position and water temperature via daily satellite passes.

Nexus-01 Edge-AI Onboard Computer

• Compute moduleNVIDIA Jetson TX2i
• CUDA cores256
• Peak performance1.3 TFLOPS

Space-qualified Edge-AI onboard computer flying on the Nexus-01 mission, processing hyperspectral imagery and running AI/ML models in orbit.

OPERA 12U/16U Cubesat Deployer

• Form factor12U/16U
• DesignLightweight
• Lateral clearanceHigh

12U/16U CubeSat deployer with lightweight design, redundant non-pyrotechnic actuation and dynamic clamping.

MASTER II Next Generation Satellite OBC

• ArchitectureModular, separated control and computing layers
• RedundancyDual-section (A/B), active/standby or dual-active modes
• FailoverHardware-driven, deterministic, no software boot required

Next-generation modular OBC with dual-section hardware redundancy, PolarFire SoC, FPGA guardian supervision and on-demand edge AI.

MASTER-CHIEF Extended On-Board Computer

• ProcessorDual core: Cortex M7 480MHz + Cortex M4 240MHz
• Critical data coreIndependent Cortex M7 400MHz
• Critical data RAM1MB with ECC

Extended CubeSat OBC adding an independent critical-data-management core with ECC RAM to the MASTER architecture.

MASTER Cubesat On-Board Computer

• ProcessorDual core: Cortex M7 480MHz + Cortex M4 240MHz
• SoftwareOTA update, FreeRTOS-compatible architecture
• Communication interfaces13x: CAN, RS422, RS485, UART, USART, I2C, SPI

Dual-core CubeSat OBC with Cortex M7/M4 processors, OTA updates, FreeRTOS compatibility and rich I/O.

CHORUS Deployable Antennas

• Form factor range1U to 16U
• Frequency bandsUHF or VHF
• Layout optionsLinear double-dipole or turnstile

Deployable CubeSat antennas from 1U to 16U, configurable in UHF or VHF with triple-redundant deployment.

SOLO Cubesat EPS

• Form factor range1U to 27U
• FunctionsPower distribution, battery management, solar array conditioning
• ArchitectureFault-tolerant, integrated PDCU

End-to-end power module for nanosatellites, combining power distribution, battery management and solar array conditioning.

DROP Deployable Solar Panels

• Form factor range1U to 16U
• ConfigurationDual, triple, or multi-wing
• Solar cellsSingle-sided or double-sided option

Deployable CubeSat solar panels from 1U to 16U with dual, triple or multi-wing configurations.

Ultra High-Pressure Composite Type IV Tank

• Tank TypeUltra high-pressure gas composite Type IV (plastic liner, resin-impregnated carbon fiber winding)
• ApplicationsHydrogen trailer cylinder bundles, hydrogen station tanks, fuel cell drones
• Stationary ApplicationKHK certification and mass production start, 2025

Ultra high-pressure gas composite Type IV tank with plastic liner and resin-impregnated carbon fiber winding, for hydrogen and…

Linerless Cryogenic Composite Tank

• Tank TypeLinerless cryogenic liquid composite tank
• ApplicationsLH2, LNG, LOX single- and double-layer vessels
• R&D / POC PhaseSingle/double layer LH2, LNG, LOX (to be installed in Space Walker's rocket)

Ultra-lightweight linerless cryogenic liquid composite propellant tank developed for SPACE WALKER's rockets, adaptable to hydrogen/LNG/LOX storage on Earth.

Two Stage To Orbit (TSTO) Vehicle

• MissionPoint-to-Point Transport / Space Travel
• Scheduled Launch Date2040s
• Vehicle TypeTwo Stage To Orbit (TSTO)

Long-term two-stage-to-orbit winged vehicle concept for point-to-point transport and orbital space travel, planned for the 2040s.

NagaTomo Space Tourism Spaceplane

• Total Length17.7 m
• Total Width12.3 m
• Fuselage Length15.8 m

Crewed suborbital spaceplane for commercial space travel, carrying 2 crew and 6 passengers to 120 km altitude, targeted…

FuJin/RaiJin Suborbital Spaceplane

• Total Length17.7 m
• Total Width12.3 m
• Fuselage Length15.8 m

Suborbital spaceplane for science missions (FuJin) and small satellite launch to LEO/SSO (RaiJin), targeting a 2028 debut from…