Products

Four-stage solid-propellant launch vehicle with 1.5t SSO / 2t LEO capacity and 100% success rate across 10 missions

Medium-lift kerosene/LOX launch vehicle with 7.8t SSO / 12t LEO capacity, first-stage reusability planned

Heavy variant of Kinetica 2 with four boosters for 15t SSO / 22t LEO capacity

Optical ground station with sub-1m aperture and adaptive optics for co-location with data centers or tactical deployment.

Cloud-based IoT data platform for device management, data routing, and delivery of satellite-received sensor data

Largest commercial rocket testing facility in the Southern Hemisphere spanning 41,000 sq km, supporting suborbital launches, orbital re-entries, and hypersonic testing

Medium-class solid-fueled launch vehicle delivering up to 1,500 kg to LEO with a 2.2 m diameter fairing

Small-lift solid-fueled launch vehicle delivering up to 300 kg to LEO, with road-mobile rapid-response capability

End-to-end hosted payload service on the P-30 bus with launch and ground segment

Mass-produced low Earth orbit broadband communication satellites with Q/V/Ka-band capability and up to 48 Gbps total capacity

Low Earth Orbit positioning, navigation, and timing satellite system under development with JAXA

Launch and early orbit phase services with priority scheduling, pre-launch rehearsals, and rapid anomaly response

Life extension servicer for geostationary satellites, providing station-keeping and orbit maintenance via docking

Large Integrated Flexible Environment, an inflatable Vectran-fabric habitat module providing approximately 300 cubic meters of pressurized volume

Crewed capsule for orbital cargo and astronaut transport, designed for MIURA Next integration

Lunar lander under development for delivering up to 100 kg to the lunar surface

In-space refueling program with Docking and Fluid Transfer port for on-orbit propellant transfer.

NASA-funded technology demonstration satellite for testing cryogenic fluid management in LEO, including zero-loss storage and transfer

Lunar cargo orbiter under development for transporting up to 1,000 kg to Moon orbits

Medium-lift three-stage launch vehicle with 10,000 kg to LEO and 4,200 kg to GTO, used for Chandrayaan and commercial missions

Intelligent node software managing sleep/wake cycles, data buffering, uplink timing, and frequency adaptation for satellite-connected devices

Medium-class satellite bus for constellation missions. ESPA Grande compatible with 300kg+ payload mass and 1.5kW peak power. Shares over 90% design commonality with S-CLASS.

Miniaturized integrated lab systems for high-precision space experiments using microfluidic chips in CubeSat form factor

InSAR-based cloud solution for millimeter-scale ground deformation detection across cities, roads, tunnels, and bridges.