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: 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	Authors ORCID iD
Gröning, Stefan	Institut für Raumfahrtantriebe, DLR Lampoldshausen	UNSPECIFIED
Hardi, Justin	Justin.Hardi (at) dlr.de	UNSPECIFIED
Suslov, Dmitry	Dmitry.Suslov (at) dlr.de	UNSPECIFIED
Oschwald, Michael	Michael.Oschwald (at) dlr.de	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 :

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 Transport

DLR - Research area:

Raumfahrt

DLR - Program:

R RP - Raumtransport

DLR - Research theme (Project):

R - Antriebsystemtechnik - Schubkammertechnologie

Location:

Lampoldshausen

Institutes and Institutions:

Institute of Space Propulsion > Rocket Propulsion

Deposited By:

Hanke, Michaela

Deposited On:

16 Nov 2016 07:49

Last Modified:

14 Dec 2019 04:27

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