Design procedure of a turbopump test bench

Pauw, J. D. and Veggi, L. and Wagner, Bernd and Mondal, J. and Klotz, M. and Haidn, O. (2017) Design procedure of a turbopump test bench. 17th International Symposium on Transport Phenomena and Dynamics of Rotating Machinery (ISROMAC), 16. - 21. Dez. 2017, Maui, USA.

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Item URL in elib:

https://elib.dlr.de/117326/

Document Type:

Conference or Workshop Item (Speech)

Title:

Design procedure of a turbopump test bench

Authors:

Authors	Institution or Email of Authors	Author's ORCID iD
Pauw, J. D.	Lehrstuhl für Turbomaschinen und Flugantriebe, TU München, D	UNSPECIFIED
Veggi, L.	Lehrstuhl für Turbomaschinen und Flugantriebe, TU München, D	UNSPECIFIED
Wagner, Bernd	UNSPECIFIED	https://orcid.org/0000-0003-3431-5898
Mondal, J.	UNSPECIFIED	UNSPECIFIED
Klotz, M.	UNSPECIFIED	UNSPECIFIED
Haidn, O.	Lehrstuhl für Turbomaschinen und Flugantriebe, TU München, D	UNSPECIFIED

Date:

2017

Refereed publication:

Yes

Open Access:

Gold Open Access:

In SCOPUS:

In ISI Web of Science:

Status:

Published

Keywords:

turbopump, rocket Motor, rocket test bench

Event Title:

17th International Symposium on Transport Phenomena and Dynamics of Rotating Machinery (ISROMAC)

Event Location:

Maui, USA

Event Type:

international Conference

Event Dates:

16. - 21. Dez. 2017

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

Deposited By:

Hanke, Michaela

Deposited On:

14 Dec 2017 08:14

Last Modified:

01 Dec 2018 19:53

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