Design, Development Evolution of an Ethanol/LOX Injection Head for Rocket Steam Generator of High Flowrate
Krühsel, G. and 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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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.
|Document Type:||Conference or Workshop Item (Paper)|
|Additional Information:||LIDO-Berichtsjahr=2003, monograph_id=AIAA 2003-5044,|
|Title:||Design, Development Evolution of an Ethanol/LOX Injection Head for Rocket Steam Generator of High Flowrate|
|Journal or Publication Title:||39th Joint Propulsion Conference and Exhibit|
|Event Title:||39th AIAA/ASME/SAE/ASEE Joint Propulsion Conference, Huntsville, AL, 20 - 23 July 2003|
|Organizer:||American Institute of Aeronautics and Astronautics|
|HGF - Research field:||Aeronautics, Space and Transport|
|HGF - Program:||Space|
|HGF - Program Themes:||W RP - Raumtransport|
|DLR - Research area:||Space|
|DLR - Program:||W RP - Raumtransport|
|DLR - Research theme (Project):||E -- no assignement|
|Institutes and Institutions:||Institute of Space Propulsion|
|Deposited By:||Monika Lohmiller|
|Deposited On:||16 Sep 2005|
|Last Modified:||06 Jan 2010 14:03|
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