Titel: |
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Autor(en): |
C. Bach, J. Sieder, O. Przybilski, M. Tajmar |
Zusammenfassung: |
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. |
Veranstaltung: |
Deutscher Luft- und Raumfahrtkongress 2013, Stuttgart |
Verlag, Ort: |
Deutsche Gesellschaft für Luft- und Raumfahrt - Lilienthal-Oberth e.V., Bonn, 2013 |
Medientyp: |
Conference Paper |
Sprache: |
englisch |
Format: |
21,0 x 29,7 cm, 10 Seiten |
URN: |
urn:nbn:de:101:1-2013112910686 |
Stichworte zum Inhalt: |
liquid propulsion, sounding Rocket |
Verfügbarkeit: |
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Kommentar: |
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Veröffentlicht am: |
29.11.2013 |