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

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

Full text not available from this repository.

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
Deeken, J.	Jan.Deeken@dlr.de
Haidn, O.	Oskar.Haidn@dlr.de
Schlechtriem, S.	Stefan.Schlechtriem@dlr.de
Suslov, D.	Dmitry.Suslov@dlr.de

Date:

2011

Journal or Publication Title:

EUCASS

Refereed publication:

Yes

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

HGF - Program:

Space

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:

Michaela Hanke

Deposited On:

16 Dec 2010 12:45

Last Modified:

13 Dec 2011 08:31

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