COMPARISON OF OXYGEN-HYDROGEN COMBUSTION VISUALISION TECHNIQUES UNDER REPRESENTATIVE CONDITIONS

Webster, Samuel and Hardi, Justin and Oschwald, Michael (2016) COMPARISON OF OXYGEN-HYDROGEN COMBUSTION VISUALISION TECHNIQUES UNDER REPRESENTATIVE CONDITIONS. In: Proceedings. Space Propulsion 2016, 2016-05-02 - 2016-05-06, Rome, Italy.

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Item URL in elib:

https://elib.dlr.de/107822/

Document Type:

Conference or Workshop Item (Speech)

Title:

COMPARISON OF OXYGEN-HYDROGEN COMBUSTION VISUALISION TECHNIQUES UNDER REPRESENTATIVE CONDITIONS

Authors:

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

Date:

2016

Journal or Publication Title:

Proceedings

Refereed publication:

Yes

Open Access:

Yes

Gold Open Access:

In SCOPUS:

In ISI Web of Science:

Status:

Published

Keywords:

liquid propellant rocket engine, combustion instability, optical diagnostics, flame visualisation, cryogenic propellants

Event Title:

Space Propulsion 2016

Event Location:

Rome, Italy

Event Type:

international Conference

Event Start Date:

2 May 2016

Event End Date:

6 May 2016

Organizer:

3AF

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 07:56

Last Modified:

24 Apr 2024 20:12

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