Space Hardware Marketplace

MIL-C-26482 Series II Circular Connector

• StandardMIL-C-26482 Series II
• Part Number ExampleMS 3474 W 18-6 P N
• Shell Types3470 (narrow flange receptacle), 3471 (cable connecting), 3472 (wide flange), 3474 (jam nut), 3475 (RFI shielding plug), 3476 (straight plug)

Upgraded bayonet-coupled MIL-C-26482 Series II circular connector with PCB contact options.

MIL-C-26482 Series I Circular Connector

• StandardMIL-C-26482 Series I
• Part Number ExampleMS 3110 E 18-32 P N L
• Shell Types3110 (wall mount), 3111 (cable), 3112 (box mount), 3114 (jam nut), 3116 (plug), 3117 (bulkhead)

Bayonet-coupled military circular connector with solder contacts conforming to MIL-C-26482 Series I.

Taiki Space Community Center SORA — Visitor & Educational Facility

• LocationBisei 169, Taiki-cho, Hiroo-gun, Hokkaido (Multipurpose Aerospace Park)
• Opening hours (Apr–Oct)10:00–16:00
• Opening hours (Nov)10:00–15:00

Free public exhibition center at Hokkaido Spaceport showcasing 40 years of aerospace development in Taiki Town, featuring MOMO…

MIL-C-5015 Series Circular Connector

• StandardMIL-C-5015
• Part Number ExampleMS 3106 A 18 10 P Y
• Shell Types3100 (wall mount receptacle), 3101 (in-line receptacle), 3102 (box mount receptacle), 3106 (straight plug), 3108 (elbow plug)

Military standard circular connectors in 5 service classes and 14 shell sizes, conforming to MIL-C-5015.

Aerospace Experiment & Research Support Services

• LocationTaiki-cho, Hiroo-gun, Hokkaido, Japan
• Disciplines supportedSuborbital rockets, high-altitude balloons, UAV/drones, eVTOL, small aircraft, rocket engine testing, university research
• Balloon operations since2008

Multi-discipline aerospace research and experimentation platform at Hokkaido Spaceport supporting suborbital rockets, high-altitude balloons, drones, eVTOL, and university…

Engine Firing Test Facility — Rocket Propulsion Testing

• LocationLaunch Complex 0 (LC0), Bisei, Taiki-cho, Hiroo-gun, Hokkaido, Japan
• Facility typeStatic fire / rocket engine firing test
• Propellants availableLNG (CH4), LOX, GHe, LN2, GN2, GOX, Water, Electrical Power

Dedicated rocket engine firing test facility at Launch Complex 0 in Taiki, Hokkaido, supporting propulsion development and qualification…

Baize Integrated Electronics System

• FunctionsAttitude control, power management, thermal control, telemetry/telecommand, health monitoring
• ArchitectureHighly integrated single-board avionics platform
• SoftwareAdvanced software architecture with in-orbit reconfiguration support

The Baize Integrated Electronics System is Hongqing Technology onboard satellite avionics platform, serving as the mission commander for…

Chiyu Solar Energy System

• TypeDeployable solar wing / solar array
• ConfigurationsSingle-wing, dual-wing
• Power Output Range1,000 W - 8,000 W

The Chiyu Solar Energy System is Hongqing Technology high-performance solar wing product line designed for LEO satellite platforms.…

Runway & Hangars — Horizontal Launch & Aerial Test Facility

• Runway dimensions1,300 × 30 m (asphalt paved)
• Orientation82°14'42" / 262°14'42"
• Design classificationLA-4

1,300-meter paved runway with two equipped hangars in Taiki, Hokkaido, supporting spaceplane operations, UAV/drone testing, eVTOL trials, and…

Jinwu Electric Propulsion System

• PropellantArgon (Ar)
• In-Orbit Ignition Cycles4,089 (verified as of June 8, 2026)
• Ignition Success Rate100%

The Jinwu Electric Propulsion System is Hongqing Technology next-generation argon-fueled electric propulsion platform, developed entirely in-house for commercial…

Launch Complex 1 (LC1) — Small Orbital Rocket Launch Site

• LocationTaiki-cho, Hiroo-gun, Hokkaido, Japan
• Latitude42.30°N
• Longitude143.26°E

Under-development orbital launch site at Hokkaido Spaceport with two launch pads (LP11, LP12), assembly buildings, and full propellant…

Scientific Experimental Satellite

• OrbitLow Earth Orbit (LEO)
• Payload InterfaceOpen, customizable for research experiments
• Data InterfaceStandardized open interfaces for global research teams

Hongqing Technology scientific experimental satellite platform provides Space as a Service for global research institutions, universities, and scientific…

Launch Complex 0 (LC0) — Suborbital Launch Services

• LocationBisei, Taiki-cho, Hiroo-gun, Hokkaido, Japan
• Latitude42.30°N
• Longitude143.26°E

Operational suborbital rocket launch site in Taiki, Hokkaido, with extensive flight heritage hosting MOMO sounding rockets and CAMUI…

Next-Generation Intelligent Remote Sensing Satellite

• OrbitLow Earth Orbit (LEO)
• Onboard AI Computing Power>=200 TOPS @ INT8 per satellite node
• Laser Inter-Satellite Link Speed>=100 Gbps

Hongqing Technology next-generation intelligent remote sensing satellite represents a paradigm shift from traditional sky sensing and ground computing…

Next-Generation LEO Broadband Communication Satellite

• OrbitLow Earth Orbit (LEO)
• ArchitectureIntegrated flat-panel antenna-platform design
• Communication LinksInter-satellite links, satellite-to-ground feeder links, satellite-to-user terminal links

Hongqing Technology next-generation low-Earth orbit broadband communication satellite is built on a self-developed low-cost, high-reliability, high-performance satellite platform.…

DNLV (Domino Next Launch Vehicle)

Malaysia's first commercially developed orbital small launch vehicle under development by Independence-X Aerospace.

MERCAP Re-entry Capsule

Malaysian microgravity experimental re-entry capsule for in-space research with sample return capability.

HIRCOM CubeSat UHF Transceiver

Radiation-resistant, CubeSat-compliant half-duplex UHF transceiver for space-to-ground TMTC links.