Combustion efficiency of a porous injector during throttling of a LOX/H2 combustion chamber

Deeken, Jan C. and Haidn, Oskar and Schlechtriem, S. and Suslov, Dmitry (2011) Combustion efficiency of a porous injector during throttling of a LOX/H2 combustion chamber. In: EUCASS Advances in Aerospace Sciences, Vol. 2 - Propulsion Physics. pp. 251-264.

Full text not available from this repository.

Item URL in elib:

https://elib.dlr.de/67717/

Document Type:

Book Section

Title:

Combustion efficiency of a porous injector during throttling of a LOX/H2 combustion chamber

Authors:

Authors	Institution or Email of Authors	Author's ORCID iD	ORCID Put Code
Deeken, Jan C.	UNSPECIFIED	https://orcid.org/0000-0002-5714-8845	UNSPECIFIED
Haidn, Oskar	UNSPECIFIED	UNSPECIFIED	UNSPECIFIED
Schlechtriem, S.	UNSPECIFIED	UNSPECIFIED	UNSPECIFIED
Suslov, Dmitry	UNSPECIFIED	https://orcid.org/0000-0002-5160-9292	UNSPECIFIED

Date:

2011

Refereed publication:

Yes

Open Access:

Gold Open Access:

In SCOPUS:

In ISI Web of Science:

Volume:

Vol. 2 - Propulsion Physics

Page Range:

pp. 251-264

Series Name:

EUCASS Advances in Aerospace Sciences

Status:

Published

Keywords:

combustion, porous injector, H2/O2

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

Deposited By:

Hanke, Michaela

Deposited On:

16 Dec 2010 12:45

Last Modified:

28 Mar 2023 23:39

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