A rocket engine used to power the Hs 293 glide bomb, an example of the use of unconventional propulsion systems.
The originality of this engine lay in the elimination of the combustion process (a so-called cold rocket engine). The propellant consisted of two components — an aqueous solution of calcium or potassium permanganate and 80% hydrogen peroxide. The catalytic reaction of permanganate with hydrogen peroxide produced an enormous amount of steam at a temperature of 500 degrees C (a so-called cold chemical reaction).
| Operating time | 10 s |
| Thrust | 590 kG |
