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CARS Temperature Measurements in a Cryogenic LOX/GH2/LH2 Rocket Combustion Chamber

Klimenko, D.N. and Clauss, Walter and Oschwald, Michael (2002) CARS Temperature Measurements in a Cryogenic LOX/GH2/LH2 Rocket Combustion Chamber. ECONOS European Conference on Nonlinear Optical Spectroscopy, 2002-03-18 - 2002-03-19, Villigen (Schweiz).

Full text not available from this repository.

Abstract

Development of liquid rocket engines is still a big challenge for the manufacturers. In the past, the design relied on accumulated know-how and trial and error methods. More recently, numerical tools have been introduced in the design process but could not replace testing. Combustion in rocket engines fed with both liquid oxygen and hydrogen at high pressure (up to 30 MPa) is so complex that modeling and simulation cannot be carried out without extensive validation based on detailed investigation of elementary processes (liquid propellant injection, atomization, droplet vaporization, turbulent mixing, combustion) in well defined configurations and nevertheless representative operating conditions.

Item URL in elib:https://elib.dlr.de/53269/
Document Type:Conference or Workshop Item (Speech, Poster)
Title:CARS Temperature Measurements in a Cryogenic LOX/GH2/LH2 Rocket Combustion Chamber
Authors:
AuthorsInstitution or Email of AuthorsAuthors ORCID iD
Klimenko, D.N.UNSPECIFIEDUNSPECIFIED
Clauss, WalterUNSPECIFIEDUNSPECIFIED
Oschwald, MichaelUNSPECIFIEDUNSPECIFIED
Date:2002
Refereed publication:No
Open Access:No
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:No
Keywords:CARS
Event Title:ECONOS European Conference on Nonlinear Optical Spectroscopy
Event Location:Villigen (Schweiz)
Event Type:international Conference
Event Dates:2002-03-18 - 2002-03-19
HGF - Research field:Aeronautics, Space and Transport (old)
HGF - Program:Space (old)
HGF - Program Themes:W - no assignment
DLR - Research area:Space
DLR - Program:W - no assignment
DLR - Research theme (Project):W - no assignment (old)
Location: Lampoldshausen
Institutes and Institutions:Institute of Space Propulsion > Technologie
Deposited By: Oschwald, Dr.rer.nat. Michael
Deposited On:16 Feb 2008
Last Modified:27 Apr 2009 14:43

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