Products

System for producing, liquefying, and storing oxygen and hydrogen propellants from lunar polar resources

Satellite-delivered emergency alert service enabling governments and MNOs to send cell broadcast alerts to mobile phones in areas without terrestrial coverage

Direct-to-device satellite connectivity service providing SMS, voice, emergency alerts, and data to unmodified mobile phones via LEO nanosatellites

Modular satellite platform for 350-800 kg payloads with integrated power and thermal management.

Large satellite bus for earth-observation and communications missions. Supports 1,000kg+ payload mass and 8+kW peak power. Shares 75% technology with S-CLASS and LX-CLASS.

Liquid oxygen/methane cryogenic upper-stage engine under development for Vega E

12U nanosatellite bus for higher-capacity payloads including Earth observation and communications

16U nanosatellite bus supporting payloads up to 21.5 kg with X-band downlink capability

3U CubeSat nanosatellite bus for compact payload missions

6U nanosatellite bus, the most widely deployed platform with flight heritage across IoT, defense, and science missions

8U nanosatellite bus for missions requiring additional payload volume

Exploration-class autonomous lunar rover for prospecting, science payloads, and surface mobility on annual missions

Maritime analytics platform for processing and fusing SAR and AIS data into actionable intelligence

Mars Atmosphere and Volatile Evolution orbiter studying the Martian upper atmosphere and its interaction with the solar wind to understand atmospheric loss since 2014

Web-based mission planning suite with orbit design, coverage analysis, and report generation

Single-stage suborbital launch vehicle for microgravity research, 100 kg payload capacity to 150 km apogee

Two-stage reusable orbital launcher for small satellites, powered by TEPREL-C kerosene/LOX engines

Medium-lift reusable two-stage orbital launcher with 13+ tonne payload capacity, in R&D phase

Multi-layer insulation blankets for spacecraft thermal control

Martian Moons eXploration sample-return mission to Phobos, planned for launch in FY2026

ESPA-class microsatellite bus accommodating payloads up to 70 kg for Earth observation, communications, and constellation applications

Multispectral imaging payload for environmental monitoring and agriculture

Partially reusable two-stage mini-launcher delivering 500-1,500 kg to LEO/SSO, powered by Prometheus methane/LOX engines

High-agility, rad-hard spacecraft platform for GEO/MEO precision rendezvous and proximity operations, docking, and on-orbit refueling.