J. Sieder, C. Bach, M. Nürmberger, N. Voigt, O. Przybilski, M. Tajmar

The SMART Rocket Project commits itself to the development and flight of a liquid propelled sounding rocket. The envisaged LOX/Ethanol rocket engine is unique within the DLR STERN student education programme. First steps towards the engine development are presented, starting with first concepts. The test bench needed for the characterization of the engine is described, followed by test combustion chambers for material and load analyses. First characterization tests were conducted and are presented. The launch of the rocket is planned for 2016.

Deutscher Luft- und Raumfahrtkongress 2014, Augsburg

Deutsche Gesellschaft für Luft- und Raumfahrt - Lilienthal-Oberth e.V., Bonn, 2015

Conference Paper

englisch

21,0 x 29,7 cm, 9 Seiten

urn:nbn:de:101:1-2015021323510

Brennkammer, Flüssigtreibstoffe

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13.02.2015