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Injection Effects in Hybrid Rocket Engines

Kobald, M. and Ciezki, H. and Schlechtriem, S. and Willerding, T. and Schindler, A. and Kott, M. and Hahn, M. (2012) Injection Effects in Hybrid Rocket Engines. In: Proceedings. Space Propulsion 2012, 7. - 10. Mai 2012, Bordeaux, France.

Full text not available from this repository.

Abstract

There exists a growing interest in Hybrid rocket engines over the last years. Lots of research has been done on hybrids in general and on topics like combustion efficiency and stability in detail. But only minor work has been done on the design and performance of the injector type. This is especially important since combustion stability can be closely linked to the type of injector and configuration of the pre-combustion chamber. In the present paper a detailed review on earlier work regarding combustion stability has been done. Hot flow experiments have been carried out to evaluate the performance of different injector types including impingement, showerhead and swirl injectors. Characteristic velocity, ISP efficiency and regression rates during hot fire tests are evaluated and compared. Combustion stability is evaluated by means of Fast-Fourier Transformations and spectrograms of the pressure signals. Impingement injectors with high impingement angles produce unstable flow fields which excite vortex shedding and the Helmholtz acoustic mode of the combustion chamber.

Document Type:Conference or Workshop Item (Speech, Paper)
Title:Injection Effects in Hybrid Rocket Engines
Authors:
AuthorsInstitution or Email of Authors
Kobald, M.Mario.Kobald@dlr.de
Ciezki, H.Helmut.Ciezki@dlr.de
Schlechtriem, S.Stefan.Schlechtriem@dlr.de
Willerding, T.DGLR Stuttgart
Schindler, A.DGLR Stuttgart
Kott, M.DGLR Stuttgart
Hahn, M.DGLR Stuttgart
Date:2012
Journal or Publication Title:Proceedings
Refereed publication:Yes
In ISI Web of Science:No
Status:Published
Keywords:hybrid rocket engines, injection effects, combustion efficiency
Event Title:Space Propulsion 2012
Event Location:Bordeaux, France
Event Type:international Conference
Event Dates:7. - 10. Mai 2012
Organizer:3AF, ESA, CNES
HGF - Research field:Aeronautics, Space and Transport
HGF - Program:Space
HGF - Program Themes:Space Transport
DLR - Research area:Raumfahrt
DLR - Program:R RP - Raumtransport
DLR - Research theme (Project):R - Antriebsystemtechnik - Schubkammertechnologie
Location: Lampoldshausen
Institutes and Institutions:Institute of Space Propulsion > Treibstoffe
Deposited By: Melanie Schmidt
Deposited On:08 Oct 2012 20:36
Last Modified:04 Nov 2012 09:19

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