All-composite pressure vessels for cryogenic fluid storage and high pressure applications

All-composite spacecraft propellant tanks (including bladder)

Unibody Composite Structures- Tanks with modified structural additions for special applications

Tridyne High Performance Pressurization System

All-composite ablative rocket engines (left- 20 Klbf thrust, right- 5 Klbf thrust)

Complete Propulsion System for Pressure-Fed Launch Vehicles

Complete Launch Systems for All Payload Classes, from Suborbital to Medium- and Heavy-lift orbital payloads, based on
proven core technologies that have undergone significant testing previously*


*Non-recurring Engineering (NRE) Development Still Required for All Vehicles at significantly lower cost than
traditional launch vehicle NRE costs , Leading to Very Low Recurring Cost Launch Systems for a given Payload Class