Braunschweig

A test facility for rocket ignition

Trauen

27 January 2014

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DLR engineers research tomorrow's hybrid engines

The concrete tube stretching across the German Aerospace Center (Deutsches Zentrum für Luft- und Raumfahrt; DLR) site in Trauen might only be 3.3 metres wide, but every now and then it becomes outer space for around 10 seconds. This is the case when engineers at the DLR Institute of Aerodynamics and Flow Technology put their newly developed hybrid rocket engine through its paces. Ognjan Božić and his team take their seats behind the 20-centimetre-thick, reinforced concrete walls in the control room while, in the test stand, liquid hydrogen peroxide reacts with solid fuel in a combustion chamber producing 240 kilograms of thrust in the rocket engine. The first analyses of the Advanced Hybrid Rocket Engine Simulation (AHRES) project show that it might take just five to 10 years to develop an airworthy hybrid engine to launch a rocket into space.

By combining a solid propellant and liquid oxidiser in one engine, the DLR researchers hope to benefit from the advantages of both systems: "They are easier to build and handle than liquid propellant engines, which makes them less costly, and the fuels are not toxic," says DLR engineer Daniel Lancelle, listing the advantages. "You can control the thrust and ignite or switch off the engine as needed. The risk of explosion is also reduced in comparison with other engines." But the scientists are aware of the drawbacks of a hybrid engine – a lower combustion rate and reduced thrust. "At the moment we are working on understanding this new kind of engine and on improving the combustion rate and engine efficiency," explains Božić. "And so far the results are promising."

Unique test facility assembled

A team comprised of DLR staff and students took it upon themselves to give the test stand at the DLR site in Trauen – unused for some 30 years – a makeover, installing state-of-the-art technology. Their purpose was to demonstrate that the hybrid rocket engine they had designed could work at least as efficiently as standard solid propellant engines. "You will not find another facility like this one in Europe," emphasises Ognjan Božić. The remote location of Trauen complies with all the safety standards required to plan future tests on larger engines with a thrust of up to 15 tons. Here, the engineers conduct tests with various solid fuels, modify the mixtures and analyse the course of combustion. The test results are then used to optimise the computer simulations.

Research at an altitude of over 40 kilometres

This type of hybrid rocket engine could, for example, be used as the upper stage of a small to medium-sized launcher. "They can be deployed in research rockets and research aircraft operating at an altitude ranging from 40 to 180 kilometres – and therefore bridge the gap between airplanes and satellites," says project manager Božić. They could also be used for spacecraft landings on the Moon and Mars. Their high degree of safety due to the separation of the different fuels before ignition opens up yet another field of application: space tourism.

"Our objective is to use the results obtained to develop engineering software that could be used by industry or research institutions to design this kind of engine or improve an existing design in just a few weeks," says DLR engineer Dennis Porrmann. Ognjan Božić, Daniel Lancelle and Dennis Porrmann plan to conduct at least five more trials by mid-2015.

Last modified:
27/01/2014 11:14:46

Contacts

 

Manuela Braun
German Aerospace Center (DLR)

Corporate Communications, Editor, Human Space Flight, Space Science, Engineering

Tel.: +49 2203 601-3882

Fax: +49 2203 601-3249
Ognjan Bozic
German Aerospace Center (DLR)

DLR Institute of Aerodynamics and Flow Technology

Tel.: +49 531 295-3326