Analysis of a transpiration cooled LOX/CH4 rocket thrust chamber

Munk, David and Selzer, Markus and Seiler, Helge and Ortelt, Markus and Vio, Gareth (2021) Analysis of a transpiration cooled LOX/CH4 rocket thrust chamber. International Journal of Heat and Mass Transfer. Elsevier. doi: 10.1016/j.ijheatmasstransfer.2021.121986. ISSN 0017-9310.

Full text not available from this repository.

Item URL in elib:

https://elib.dlr.de/145754/

Document Type:

Article

Title:

Analysis of a transpiration cooled LOX/CH4 rocket thrust chamber

Authors:

Authors	Institution or Email of Authors	Author's ORCID iD	ORCID Put Code
Munk, David	UNSPECIFIED	UNSPECIFIED	UNSPECIFIED
Selzer, Markus	UNSPECIFIED	https://orcid.org/0000-0003-1081-5281	UNSPECIFIED
Seiler, Helge	UNSPECIFIED	UNSPECIFIED	UNSPECIFIED
Ortelt, Markus	UNSPECIFIED	UNSPECIFIED	UNSPECIFIED
Vio, Gareth	University of Sidney	UNSPECIFIED	UNSPECIFIED

Date:

September 2021

Journal or Publication Title:

International Journal of Heat and Mass Transfer

Refereed publication:

Yes

Open Access:

Gold Open Access:

In SCOPUS:

Yes

In ISI Web of Science:

Yes

DOI:

10.1016/j.ijheatmasstransfer.2021.121986

Publisher:

Elsevier

ISSN:

0017-9310

Status:

Published

Keywords:

Transpiration cooling Computational fluid dynamics Rocket thrust chamber Ceramic matrix composites

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:

Stuttgart

Institutes and Institutions:

Institute of Structures and Design > Space System Integration

Deposited By:

Selzer, Markus

Deposited On:

17 Nov 2021 09:10

Last Modified:

22 Nov 2021 14:01

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