Influence of LOX Injector Wall Thickness on Atomization and Combustion of LOX/CH4 Sprays

Fusetti, A. and De Rosa, M. and Oschwald, M. and Haidn, O. (2006) Influence of LOX Injector Wall Thickness on Atomization and Combustion of LOX/CH4 Sprays. In: ICLASS 2006, ICLASS. ICLASS 2006, 2006-08-27 - 2006-09-01, Kyoto (Japan).

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Item URL in elib:

https://elib.dlr.de/48120/

Document Type:

Conference or Workshop Item (Speech, Paper)

Title:

Influence of LOX Injector Wall Thickness on Atomization and Combustion of LOX/CH4 Sprays

Authors:

Authors	Institution or Email of Authors	Author's ORCID iD
Fusetti, A.	UNSPECIFIED	UNSPECIFIED
De Rosa, M.	UNSPECIFIED	UNSPECIFIED
Oschwald, M.	UNSPECIFIED	UNSPECIFIED
Haidn, O.	UNSPECIFIED	UNSPECIFIED

Date:

2006

Journal or Publication Title:

ICLASS 2006

Refereed publication:

Yes

Open Access:

Yes

Gold Open Access:

In SCOPUS:

In ISI Web of Science:

Yes

Volume:

ICLASS

Status:

Published

Keywords:

rocket, combustion, propellant injection

Event Title:

ICLASS 2006

Event Location:

Kyoto (Japan)

Event Type:

international Conference

Event Dates:

2006-08-27 - 2006-09-01

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:

22 May 2007

Last Modified:

31 Jul 2019 19:19

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