Aerospace Engines A to Z
Aerospace Engines A to Z

Updated: 21-Jun-2025

TECHNICAL UNIVERSITY MUNCHEN (TUM)

(Germany)


TECHNICAL UNIVERSITY MUNCHEN (TUM) engine specifications

Among many projects, the WARR engine was tested on a Barbarella I rocket.

The Barbarella, complete and combustion chamber
"The Barbarella, complete, and combustion chamber"

Hybrid engine test
"Hybrid engine test"

Engines of TECHNICAL UNIVERSITY MUNCHEN (TUM)

Model: WARR rocket engine

Arquitecture:
Chambers:
Fuels:
Feed System:
Ignition:
Thrust:
Weight:

Other details: