25,000 lbf dual expander cycle engine developed through DARPA XS-1 and NASA Tipping Point programs — additively manufactured aluminum metal matrix composite thrust chamber, just three parts.
Broadsword Rocket Engine
25,000 lbf dual expander cycle engine developed through DARPA XS-1 and NASA Tipping Point programs — additively manufactured aluminum metal matrix composite thrust chamber, just three parts.
Description
Broadsword is Masten's next-generation 25,000 lbf thrust dual expander cycle rocket engine, developed through the DARPA XS-1 program and further matured through a NASA Tipping Point contract. It features a custom-developed aluminum metal matrix composite thrust chamber assembly, additively manufactured using just three parts, enabling a low-cost solution for reusable launch vehicles.
Specifications
| Thrust | 25,000 lbf |
|---|---|
| Cycle | Dual expander |
| Propellants | Liquid Oxygen / Methane |
| Programs | DARPA XS-1, NASA Tipping Point |
| Thrust chamber material | Aluminum metal matrix composite (additively manufactured, 3 parts) |