Products

Partially reusable liquid-fueled launch vehicle with 25,600 kg LEO capacity, powered by nine Yuanli-110 kerosene-LOX engines

Planned heavy-lift variant using three Gravity-2 cores with 30,600 kg LEO capacity

90,000 sq ft spacecraft manufacturing capability across facilities in Centennial, CO and Long Beach, CA for high-rate spacecraft production.

ASCENT-fueled thruster with patented monolithic catalyst, replacing toxic hydrazine

Medium-class lunar lander with 625 kg payload capacity, targeting lunar south pole missions at $1.2M/kg to surface

Ground-based multi-modal sensor system for LEO space domain awareness using electro-optical, event-based, and polarimetric sensing, observing up to 10% of the LEO catalog per day.

System enabling existing utility-scale solar projects to receive and convert near-infrared light from orbit into grid electricity

Portable ground stations that receive infrared laser power from orbiting satellites

Managed ground station services including antenna hosting, radio licensing, frequency coordination, and infrastructure management for satellite operators seeking turnkey ground segment access.

LEO tracking stations with S/X-band and VHF/UHF antennas across 13 stations globally

Nine ground stations in seven global locations supporting S-band, X-band, and Ka-band uplink/downlink.

Global network of 10+ owned and 11 partner satellite ground stations providing TT&C, LEOP support, data reception, and teleport services across S, X, Ka, and optical bands.

Shared and dedicated ground station access across a global network supporting all major frequency bands

Medium-lift liquid-fueled launch vehicle replacing the H-IIA series, launched from Tanegashima Space Center

Modular lunar lander platform used for Missions 1 and 2, designed for low-cost payload delivery to the lunar surface.

Two-stage launch vehicle (22.5 m, 1.4 m diameter) with methane-LOX upper stage and kick stage, delivering 170 kg to 500 km SSO

Three-stage launch vehicle (39.6 m, 3.7 m diameter) with nine hybrid engines on the first stage, capable of delivering 1,300 kg to 500 km SSO

Two-stage small satellite launch vehicle (21.8 m, 1.4 m diameter) capable of delivering 50-90 kg to 500 km SSO using a 25-ton hybrid first stage and selectable hybrid or methane second stage

Single-stage suborbital test launch vehicle with 150 kN hybrid rocket engine; successfully launched from Alcantara Space Center in March 2023

High-Altitude Platform Stations for persistent surveillance and communications from the stratosphere

Turnkey deployable observatory sensor system for space surveillance training and operations

360-degree wireless power transmission demonstrator that proved retrodirective beam steering for space-to-ground energy transfer

Suborbital launch vehicle derived from Electron for hypersonic flight testing. Deploys payloads up to 700 kg at velocities from 3 to 7.5+ km/s and altitudes above 80 km. 7 launches with 100% mission success.

Complete hypersonic missile system powered by Draper engine with in-house solid rocket motor booster