Liquid Fuel Rocket Engine 150 N

This engine uses one single catalytic propellant which is hydrogen peroxide and ceramic catalizer.

The dynamic thrust is about 150 N, and this is a "cold" engine built in aluminium that has an excellent dynamic thrust-weight rate.

“The same natural forces, which make us possible to fly to the stars put us also into the position to destroy our star.”
Wernher Magnus Maximilian von Braun