America's First Ox-Rich Staged Combustion Engine
5,000 lbf
Thrust, Sea Level
Lox / Kerosene
Propellants
Reusable
Low Earth Orbit, Geostationary Orbit, In-Space, Hypersonics
Hadley
In Production
Our one-of-a kind campus co-locates engineering, manufacturing, & testing operations, allowing for unmatched development time and the chance for employees, customers, and investors alike to experience rocket engine testing as a part of the normal work day.
Specifications
5,000 lbf
Ox-rich Staged Combustion
Thrust, Sea Level
Lox / Kerosene
Propellants
Reusable
Low Earth Orbit Geostationary Orbit In-Space Hypersonics
>200s
Continuous burn at rated power
>600s
Qualified Engine Life
±7°
Max Gimbal Angle
EXPLORE OUR ENGINES
in development
Draper
4,000
lbf
Closed Catalyst Cycle
Thrust, Sea Level
Hydrogen Peroxide/Kerosene
Propellants
Reusable
HypersonicsDefense
in development
In Development
Ripley
50,000
lbf
Ox-rich Staged Combustion
Thrust, Sea Level
Lox / Kerosene
Propellants
Reusable
Low EarthGeostationary Orbit
In Development
In Development
Arroway
200,000
lbf
THRUST, SEA LEVEL
Lox / Methane
PROPELLANTS
Reusable
Medium & Heavy Boost
In Development