Flame dynamics of an injection element operated with LOX/H2, LOX/CNG and LOX/LNG in a sub- and supercritical rocket combustor with large optical access

Martin, Jan and Armbruster, Wolfgang and Stützer, Robert and Suslov, Dmitry and Hardi, Justin and Oschwald, Michael (2023) Flame dynamics of an injection element operated with LOX/H2, LOX/CNG and LOX/LNG in a sub- and supercritical rocket combustor with large optical access. International Journal of Spray and Combustion Dynamics. SAGE Publications. doi: 10.1177/17568277231172302. ISSN 1756-8277.

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Official URL: https://journals.sagepub.com/home/scd

Item URL in elib:

https://elib.dlr.de/200046/

Document Type:

Article

Title:

Flame dynamics of an injection element operated with LOX/H2, LOX/CNG and LOX/LNG in a sub- and supercritical rocket combustor with large optical access

Authors:

Authors	Institution or Email of Authors	Author's ORCID iD	ORCID Put Code
Martin, Jan	UNSPECIFIED	https://orcid.org/0000-0002-5050-2506	147801778
Armbruster, Wolfgang	UNSPECIFIED	https://orcid.org/0000-0002-4859-4173	147801780
Stützer, Robert	UNSPECIFIED	https://orcid.org/0000-0003-4136-8496	UNSPECIFIED
Suslov, Dmitry	UNSPECIFIED	https://orcid.org/0000-0002-5160-9292	UNSPECIFIED
Hardi, Justin	UNSPECIFIED	https://orcid.org/0000-0003-3258-5261	UNSPECIFIED
Oschwald, Michael	UNSPECIFIED	https://orcid.org/0000-0002-9579-9825	UNSPECIFIED

Date:

19 May 2023

Journal or Publication Title:

International Journal of Spray and Combustion Dynamics

Refereed publication:

Yes

Open Access:

Yes

Gold Open Access:

In SCOPUS:

Yes

In ISI Web of Science:

Yes

DOI:

10.1177/17568277231172302

Publisher:

SAGE Publications

ISSN:

1756-8277

Status:

Published

Keywords:

Rocket engine, subcritical combustion, supercritical combustion, optical access, liquid oxygen/natural gas, liquid oxygen/hydrogen, single-injector

HGF - Research field:

Aeronautics, Space and Transport

HGF - Program:

Space

HGF - Program Themes:

Space Transportation

DLR - Research area:

Raumfahrt

DLR - Program:

R RP - Space Transportation

DLR - Research theme (Project):

R - Reusable Space Systems and Propulsion Technology

Location:

Lampoldshausen

Institutes and Institutions:

Institute of Space Propulsion > Rocket Propulsion Technology
Institute of Space Propulsion > Rocket Engine Systems
Institute of Space Propulsion > Leitungsbereich RA

Deposited By:

Hanke, Michaela

Deposited On:

30 Nov 2023 15:17

Last Modified:

07 Nov 2025 11:14

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