Krühsel, G. und Schäfer, K. (2003) Design, Development Evolution of an Ethanol/LOX Injection Head for Rocket Steam Generator of High Flowrate. In: 39th Joint Propulsion Conference and Exhibit. AIAA. 39th AIAA/ASME/SAE/ASEE Joint Propulsion Conference, Huntsville, AL, 20 - 23 July 2003.
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Kurzfassung
This paper summarizes DLR design efforts and test results of an injection head of a 45 kg/s steam generator (SG) based on rocket combustion principle. Propellants in use are liquid oxygen (LOX) and ethanol (80%). Principles of design, design evolution and hot firing results are presented. Experimental investigations of combustion stability of the 45 kg/s SG in order to increase margin to combustion instability are summarised. Subjects of tests are an adjustable quarter wave tube ring and a pototype baffle. The most promising absorber type to be integrated into the SG was found to be the baffle. Design modifications of the injector design since 2001 are described.
elib-URL des Eintrags: | https://elib.dlr.de/1634/ | ||||||||||||
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Dokumentart: | Konferenzbeitrag (Paper) | ||||||||||||
Zusätzliche Informationen: | LIDO-Berichtsjahr=2003, monograph_id=AIAA 2003-5044, | ||||||||||||
Titel: | Design, Development Evolution of an Ethanol/LOX Injection Head for Rocket Steam Generator of High Flowrate | ||||||||||||
Autoren: |
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Datum: | 2003 | ||||||||||||
Erschienen in: | 39th Joint Propulsion Conference and Exhibit | ||||||||||||
Open Access: | Nein | ||||||||||||
Gold Open Access: | Nein | ||||||||||||
In SCOPUS: | Nein | ||||||||||||
In ISI Web of Science: | Nein | ||||||||||||
Herausgeber: |
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Verlag: | AIAA | ||||||||||||
Name der Reihe: | AIAA | ||||||||||||
Status: | veröffentlicht | ||||||||||||
Veranstaltungstitel: | 39th AIAA/ASME/SAE/ASEE Joint Propulsion Conference, Huntsville, AL, 20 - 23 July 2003 | ||||||||||||
Veranstalter : | American Institute of Aeronautics and Astronautics | ||||||||||||
HGF - Forschungsbereich: | Verkehr und Weltraum (alt) | ||||||||||||
HGF - Programm: | Weltraum (alt) | ||||||||||||
HGF - Programmthema: | W RP - Raumtransport | ||||||||||||
DLR - Schwerpunkt: | Weltraum | ||||||||||||
DLR - Forschungsgebiet: | W RP - Raumtransport | ||||||||||||
DLR - Teilgebiet (Projekt, Vorhaben): | E - keine Zuordnung | ||||||||||||
Standort: | Lampoldshausen | ||||||||||||
Institute & Einrichtungen: | Institut für Raumfahrtantriebe | ||||||||||||
Hinterlegt von: | Lohmiller, Monika | ||||||||||||
Hinterlegt am: | 16 Sep 2005 | ||||||||||||
Letzte Änderung: | 06 Jan 2010 14:03 |
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