Steady-State High Pressure LOX/H2 Rocket Engine Combustion

Smith, J.J. and Bechle, M. and Suslov, D. and Oschwald, M. and Haidn, O. and Schneider, G. (2005) Steady-State High Pressure LOX/H2 Rocket Engine Combustion. 1st EUCASS, 2005-07-04 - 2005-07-07, Moscow (Russia).

Preview

PDF
621kB

Item URL in elib:

https://elib.dlr.de/53351/

Document Type:

Conference or Workshop Item (Speech, Paper)

Title:

Steady-State High Pressure LOX/H2 Rocket Engine Combustion

Authors:

Authors	Institution or Email of Authors	Author's ORCID iD	ORCID Put Code
Smith, J.J.	UNSPECIFIED	UNSPECIFIED	UNSPECIFIED
Bechle, M.	UNSPECIFIED	UNSPECIFIED	UNSPECIFIED
Suslov, D.	UNSPECIFIED	UNSPECIFIED	UNSPECIFIED
Oschwald, M.	UNSPECIFIED	UNSPECIFIED	UNSPECIFIED
Haidn, O.	UNSPECIFIED	UNSPECIFIED	UNSPECIFIED
Schneider, G.	UNSPECIFIED	UNSPECIFIED	UNSPECIFIED

Date:

2005

Refereed publication:

Open Access:

Yes

Gold Open Access:

In SCOPUS:

In ISI Web of Science:

Status:

Published

Keywords:

rocket propulsion

Event Title:

1st EUCASS

Event Location:

Moscow (Russia)

Event Type:

international Conference

Event Start Date:

4 July 2005

Event End Date:

7 July 2005

HGF - Research field:

Aeronautics, Space and Transport (old)

HGF - Program:

Space (old)

HGF - Program Themes:

W RP - Raumtransport

DLR - Research area:

Space

DLR - Program:

W RP - Raumtransport

DLR - Research theme (Project):

W - Antriebsystemtechnik - Schubkammertechnologie und Hochdruckverbrennung (old)

Location:

Lampoldshausen

Institutes and Institutions:

Institute of Space Propulsion > Technologie

Deposited By:

Oschwald, Dr.rer.nat. Michael

Deposited On:

14 Nov 2008

Last Modified:

24 Apr 2024 19:16

Repository Staff Only: item control page