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Steady State High Pressure LOX / H2 Rocket Engine Combustion

Smith, J. and Schneider, Günter and Sulsov, Dmitry and Oschwald, Michael and Haidn, Oskar (2007) Steady State High Pressure LOX / H2 Rocket Engine Combustion. Aerospace Science and Technology, Vol. 11 (Issue 1), pp. 39-47.

Full text not available from this repository.


Item URL in elib:https://elib.dlr.de/53101/
Document Type:Article
Title:Steady State High Pressure LOX / H2 Rocket Engine Combustion
Authors:
AuthorsInstitution or Email of AuthorsAuthors ORCID iD
Smith, J.ExternUNSPECIFIED
Schneider, GünterUNSPECIFIEDUNSPECIFIED
Sulsov, DmitryUNSPECIFIEDUNSPECIFIED
Oschwald, MichaelUNSPECIFIEDUNSPECIFIED
Haidn, OskarUNSPECIFIEDUNSPECIFIED
Date:2007
Journal or Publication Title:Aerospace Science and Technology
Open Access:No
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:No
Volume:Vol. 11
Page Range:pp. 39-47
Status:Published
Keywords:high pressure
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
Deposited By: Hanke, Michaela
Deposited On:06 Feb 2008
Last Modified:27 Apr 2009 14:41

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