Space Hardware Marketplace

IANUS & PERSEUS Cold Gas Propulsion

Flight-proven 6 D.o.F. cold gas propulsion systems (R134a) for fine maneuvering, collision avoidance, and proximity operations.

REGULUS Electric Propulsion

Iodine-fed electric propulsion system family for small satellites, deployers, and OTVs, from 50 W to 150 W.

AxelLiner Microsatellite Development Service

• Service typeEnd-to-end: mission design → launch → operations
• Satellite classMicrosatellites
• Manufacturing facilityIn-house cleanroom, Nihonbashi, Tokyo

End-to-end microsatellite development, manufacturing, launch, and operations service for corporate and government customers seeking their own in-orbit assets.

AxelGlobe Earth Observation Service

• PlatformGRUS series optical imaging microsatellites
• Ground sampling distance~2.5 m (standard); higher resolution from GRUS-2/3
• Spectral bandsMultispectral (visible + near-infrared)

Commercial Earth observation platform providing optical satellite imagery from the GRUS microsatellite constellation for agriculture, environment, infrastructure, and…

BLACK BIRD Sounding Rocket Series

• BLACK BIRD-1 — Length1,485 mm
• BLACK BIRD-1 — Diameter105 mm
• BLACK BIRD-1 — Mass8.5 kg

Customer-configurable hybrid-propulsion sounding rockets for microgravity and atmospheric research, using liquid nitrous oxide (LN₂O) and HDPE propellants.

HANBIT-Mini Launch Vehicle

• Payload capacity1,300 kg (500 km SSO)
• Height39.6 m
• Diameter3.7 m

Three-stage small satellite launcher delivering up to 1,300 kg to 500 km SSO, powered by nine 25-ton hybrid…

HANBIT-Micro Launch Vehicle

• Payload capacity170 kg (500 km SSO)
• Height22.5 m
• Diameter1.4 m

Two-stage + kick stage small satellite launcher delivering up to 170 kg to 500 km SSO, with dual…

VOLANS Launch Vehicle

• PropulsionHybrid HTP oxidizer / HRF-1 fuel
• Payload capacityUp to 750 kg (simulated for 400 km, 40° orbit)
• Fairing length (main)2.40 m

Modular, low-cost, 100% pyrotechnics-and-explosives-free hybrid-propulsion launch vehicle carrying up to 750 kg to LEO.

VEGA Hypersonic Platform

• ConfigurationTwo-stage, fully reusable, horizontal launch
• Primary roleHypersonic research and experimental testbed
• Secondary roleSmall-satellite launcher (with expendable upper stage)

Fully reusable two-stage horizontally-launched hypersonic testbed that can also serve as a small-satellite launcher.

Future Heavy Spaceplane

• Target timeframeEarly 2030s
• ConfigurationSemi-SSTO ('1.5-stage'), evolving toward full SSTO
• ApplicationsCrew/cargo transport, satellite launch, debris removal, lunar/interplanetary payloads (with upper stage)

Roadmap concept for a fully reusable heavy orbital spaceplane, evolving step-by-step toward a single-stage-to-orbit (SSTO) vehicle.

Spaceplane Aerial Refueling System

• Refuel mediaKerosene, potentially liquid oxygen
• Program sponsorBAAINBw (since 2024)
• DemonstratorsALEDA (simulated tanker), Mini MIRA II (receiver), ORCA (scaled tanker, in manufacturing)

Optional aerial-refueling capability for POLARIS spaceplanes and hypersonic aircraft, plus dedicated uncrewed tanker aircraft.

Aurora Light Spaceplane

• Payload capacityUp to 1,000 kg to orbit
• Suborbital/hypersonic payloadUp to 10,000 kg
• ConfigurationTwo-stage-to-orbit, reusable carrier + expendable upper stage

Two-stage-to-orbit reusable spaceplane taking off and landing like an aircraft from conventional runways, carrying up to 1,000 kg…

SIRIUS Launch Vehicle Family

• ConfigurationSIRIUS 1: single central core, 2 stages
• SIRIUS 1 payload to SSO 500 km180 kg
• SIRIUS 1 payload at 50° inclination300 kg

Family of reusable dedicated small-satellite launch vehicles from Sirius Space Services, scaling from 180 kg to 1100+ kg…

ROSA Roll-Out Solar Array

Patented lightweight elastically deployable roll-out solar array for satellites and space stations.

Iris Propulsion Module

• Height< 30 cm
• Radiation tolerance30 kRad TID
• PropellantXenon or Krypton

Bolt-on solar electric propulsion module for rideshare small spacecraft.

Halo 8

• Mass0.83 kg
• Volume0.375 U
• Input Power100 – 450 W

Flight-proven Hall-effect thruster for CubeSats and small satellites, 100-450W power range.

G500 Gyroscope

• ApplicationSpacecraft attitude determination (nanosatellites, small satellites)
• FunctionAngular rate measurement
• InterfaceCompatible with standard ADCS integration

Compact gyroscope for spacecraft attitude determination in nanosatellite and small satellite missions.

Fluid-Dynamic Attitude Control System (FDA)

Fluid-dynamic attitude control system for spacecraft attitude determination and control.