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.

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

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

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 — Dedicated Nano Launch Vehicle

Malaysian indigenous LOX/RP-1 small launch vehicle — 200 kg to 500 km LEO/SSO, US$4.5M per mission, equatorial launch…

MERCAP Microgravity Experiment Re-entry Capsule

• Capsule typeUnmanned recoverable re-entry capsule
• Primary payloadLab-on-a-Chip pharma and biotech experiment specimens
• Maximum payload mass4 kg

Recoverable unmanned re-entry capsule for retrieving microgravity experiment specimens — purpose-built for Lab-on-a-Chip pharma and biotech payloads up…

HIRCOM CubeSat UHF Transceiver

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

Ka user terminal

• StatusIn development
• FundingEuropean Union’s HORIZON EIC 2023 Accelerator programme under grant agreement No 190156996

A high-performance, low-cost flat panel antenna terminal operating at Ka-band, currently under development to enable satellite-based broadband communications.

RIS Panels FR1, FR2, FR3

Reconfigurable Intelligent Surface (RIS) panels for 5G FR1, FR2, and FR3 frequency bands, enabling passive wave steering for…