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Steady-State High Pressure LOX/H2 Rocket Engine Combustion

Smith, J.J. and Bechle, M. and Suslov, D. and Oschwald, M. and Haidn, O. and Schneider, G. (2005) Steady-State High Pressure LOX/H2 Rocket Engine Combustion. 1st EUCASS, 2005-07-04 - 2005-07-07, Moscow (Russia).

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Item URL in elib:https://elib.dlr.de/53351/
Document Type:Conference or Workshop Item (Speech, Paper)
Title:Steady-State High Pressure LOX/H2 Rocket Engine Combustion
Authors:
AuthorsInstitution or Email of AuthorsAuthors ORCID iD
Smith, J.J.UNSPECIFIEDUNSPECIFIED
Bechle, M.UNSPECIFIEDUNSPECIFIED
Suslov, D.UNSPECIFIEDUNSPECIFIED
Oschwald, M.UNSPECIFIEDUNSPECIFIED
Haidn, O.UNSPECIFIEDUNSPECIFIED
Schneider, G.UNSPECIFIEDUNSPECIFIED
Date:2005
Refereed publication:No
Open Access:Yes
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:No
Status:Published
Keywords:rocket propulsion
Event Title:1st EUCASS
Event Location:Moscow (Russia)
Event Type:international Conference
Event Dates:2005-07-04 - 2005-07-07
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 > Technologie
Deposited By: Oschwald, Dr.rer.nat. Michael
Deposited On:14 Nov 2008
Last Modified:31 Jul 2019 19:21

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