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Combustion efficiency sensitivity studies of the API injector concept

Deeken, Jan C. and Suslov, Dmitry and Haidn, Oskar and Schlechtriem, S. (2011) Combustion efficiency sensitivity studies of the API injector concept. In: Proceedings (AIAA 2011-793). 49th AIAA Aerospace Sciences Meeting, 2011-01-04 - 2011-01-07, Orlando, Florida, USA.

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Since a few years DLR Lampoldshausen has been engaged in the development of a new injection concept for cryogenic liquid propellant rocket engines. This concept bases on the injection of the liquid oxygen through a large number of simple tubes while the entire hydrogen is injected through the porous face plate.3, 4 The key feature of the API concept is the independency of the atomization, vaporization, mixing and combustion performance of initial injection conditions such as velocity ratio, momentum fluxratio, Weber number or other non-dimensional parameters which are generally deemed important. This statement will be supported by data optained with a 50mm subscale combustion chamber. The influence of the velocity ratio at injection will be shown through a variation of the propellant mixture ratio and/or the chamber pressure.

Item URL in elib:https://elib.dlr.de/72139/
Document Type:Conference or Workshop Item (Speech, Paper)
Title:Combustion efficiency sensitivity studies of the API injector concept
AuthorsInstitution or Email of AuthorsAuthor's ORCID iDORCID Put Code
Deeken, Jan C.UNSPECIFIEDhttps://orcid.org/0000-0002-5714-8845UNSPECIFIED
Suslov, DmitryUNSPECIFIEDhttps://orcid.org/0000-0002-5160-9292UNSPECIFIED
Journal or Publication Title:Proceedings
Open Access:No
Gold Open Access:No
In ISI Web of Science:No
Keywords:rocket engines, combustion
Event Title:49th AIAA Aerospace Sciences Meeting
Event Location:Orlando, Florida, USA
Event Type:international Conference
Event Start Date:4 January 2011
Event End Date:7 January 2011
HGF - Research field:Aeronautics, Space and Transport (old)
HGF - Program:Space (old)
HGF - Program Themes:W RP - Raumtransport
DLR - Research area:Space
DLR - Program:W RP - Raumtransport
DLR - Research theme (Project):W - Antriebsystemtechnik - Schubkammertechnologie und Hochdruckverbrennung (old)
Location: Lampoldshausen
Institutes and Institutions:Institute of Space Propulsion > Rocket Propulsion
Institute of Space Propulsion > Technologie
Deposited By: Hanke, Michaela
Deposited On:30 Nov 2011 12:19
Last Modified:24 Apr 2024 19:37

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