Low Cost Satellite Launching
Stein Astronautics developed a 60,000 lbf Thrust Rocket Engine using LOX and Alcohol. Our Engine is based on Pintle Injector Technology, which is readily used today. We are currently developing and testing a second stage engine capable of 6,000 lbf of thrust.
Stein Astronautics has completed Ablative testing, Cold flows of the injector LOX, alcohol, and both interacting.
Stein Astronautics will design and test the components required to launch a 100 kg satellite in a 800 km polar orbit.
Second Stage Engine
Stein Astronautics is developing and testing a Second Stage Engine with capabilities of 8000 lbf of thrust with test ablative nozzles, suitable for second stage of a satellite launcher vehicle.