Rocket Lab USA

Advanced carbon composite structures and integrated assemblies for aerospace applications. Produces satellite bus structural panels, primary structures, solar panel substrates, and composite tanks across facilities in the US and New Zealand.

Small-lift orbital launch vehicle delivering up to 300 kg to LEO via 3D-printed electric-pump-fed Rutherford engines. 84 launches, 249+ satellites deployed. Second most frequently launched U.S. rocket.

Interplanetary spacecraft platform for deep space missions. Flight heritage on NASA CAPSTONE (Moon) and ESCAPADE (Mars).

Constellation-class satellite platform delivering secure, low-latency, high-speed communications connectivity in LEO. Scalable for national security operations, commercial customers, and remote sensing applications.

Flight-proven software-defined radios for telemetry, tracking, and command across L-, S-, C-, X-, and Ka-band frequencies. 13+ years of flight heritage powering missions from LEO to deep space including NASA Europa Clipper and CAPSTONE.

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.

High-power spacecraft bus designed for 12+ year lifespan with ~3 kW power. Selected for Globalstar constellation and SDA Tranche 2.

Medium-lift reusable launch vehicle (13,000 kg to LEO) powered by methane/LOX Archimedes engines. Carbon composite structure with captive Hungry Hippo fairing. In development.

Satellite payloads purpose-built for U.S. national security and intelligence missions. Delivers SWIR, MWIR, and LWIR infrared sensors with high-resolution electro-optical imaging and real-time onboard processing. Heritage from Geost with 20+ years of EO/IR innovation and 100% on-orbit mission success.

Integrated launch-plus-spacecraft solution based on modified Electron Kick Stage for responsive LEO missions.

Configurable medium delta-V spacecraft supporting payloads up to 120 kg with re-entry capability. First launched June 2023 for Varda Space Industries, returned to Earth February 2024. Fifth vehicle in development for another customer.

Standardized family of seven customizable solar array configurations ranging from 100W to 2,000+ watts. Uses quad-junction cells with up to four panels per wing, designed for short lead times and lower costs through pre-engineered configurations.

Flight-proven star trackers (185+ on orbit), reaction wheels (1,100+ on orbit), and separation systems manufactured in-house. Heritage from Sinclair Interplanetary and Planetary Systems Corp.

Radiation-hardened silicon solar cell modules and hybrid arrays designed to power gigawatt-scale space-based data centers, complementing SolAero gallium arsenide space solar products

High-efficiency space solar cells, CICs, and panels powering 1,000+ spacecraft including James Webb Space Telescope.

Flight software, mission simulation, and GNC solutions powering 80+ successful missions with 200+ cumulative years in space. Includes MAX flight software platform, Intermission ground operations, Maestro digital engineering, and SOLIS simulation environment.