Projects / ENGINES

Engine μ2

Our kerosene/LOX liquid engine

Project Overview

The μ2 Engine is built to be our first flight engine. It is the direct successor of the μ Engine, our first ever engine. Like its predecessor, μ2 features a graphite nozzle, and an ablative chamber liner. Unlike its predecessor, μ2 uses an additively manufactured triplet impinging injector. To date engine μ2 has been hot fire tested 8 times.

820 lbf

Thrust Peak

365 psia

Chamber Pressure

210 s

lsp peak