Influence of hydrogen temperature on the stability of a rocket engine combustor operated with hydrogen and oxygen

Gröning, Stefan and Hardi, Justin and Suslov, Dmitry and Oschwald, Michael (2016) Influence of hydrogen temperature on the stability of a rocket engine combustor operated with hydrogen and oxygen. CEAS Space Journal. Springer. doi: 10.1007/s12567-016-0130-8. ISSN 1868-2502.

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Item URL in elib:

https://elib.dlr.de/107791/

Document Type:

Article

Title:

Influence of hydrogen temperature on the stability of a rocket engine combustor operated with hydrogen and oxygen

Authors:

Authors	Institution or Email of Authors	Author's ORCID iD	ORCID Put Code
Gröning, Stefan	Institut für Raumfahrtantriebe, DLR Lampoldshausen	UNSPECIFIED	UNSPECIFIED
Hardi, Justin	UNSPECIFIED	https://orcid.org/0000-0003-3258-5261	UNSPECIFIED
Suslov, Dmitry	UNSPECIFIED	https://orcid.org/0000-0002-5160-9292	UNSPECIFIED
Oschwald, Michael	UNSPECIFIED	https://orcid.org/0000-0002-9579-9825	UNSPECIFIED

Date:

2016

Journal or Publication Title:

CEAS Space Journal

Refereed publication:

Yes

Open Access:

Gold Open Access:

In SCOPUS:

Yes

In ISI Web of Science:

Yes

DOI:

10.1007/s12567-016-0130-8

Publisher:

Springer

ISSN:

1868-2502

Status:

Published

Keywords:

Combustion instabilities · Hydrogen temperature ramping · Liquid propellant rocket engines

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 - Antriebsystemtechnik - Schubkammertechnologie (old)

Location:

Lampoldshausen

Institutes and Institutions:

Institute of Space Propulsion > Rocket Propulsion

Deposited By:

Hanke, Michaela

Deposited On:

16 Nov 2016 07:49

Last Modified:

21 Nov 2023 10:29

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