C. Bach, J. Sieder, O. Przybilski, M. Tajmar

Embedded within the DLR STERN programme, the SMART Rockets Project is a student mission with the aim to develop and launch a 500 N ethanol / LOX driven sounding rocket. It is right now in an early phase B project status. The constructed test bench is a cornerstone for the whole project and hence described in detail. On this basis an overview of recent test activities is given with an emphasis on the development of a first injector model. In addition to the presentation of first measurement results an analysis of the combustion chamber parameters is depicted. The final launch is envisaged for late 2015.

Deutscher Luft- und Raumfahrtkongress 2013, Stuttgart

Deutsche Gesellschaft für Luft- und Raumfahrt - Lilienthal-Oberth e.V., Bonn, 2013

Conference Paper

englisch

21,0 x 29,7 cm, 10 Seiten

urn:nbn:de:101:1-2013112910686

liquid propulsion, sounding Rocket

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29.11.2013