elib
DLR-Header
DLR-Logo -> http://www.dlr.de
DLR Portal Home | Imprint | Privacy Policy | Accessibility | Contact | Deutsch
Fontsize: [-] Text [+]

Flame Characteristics and Response of a High-Pressure LOX/CNG Rocket Combustor with Large Optical Access

Martin, Jan and Armbruster, Wolfgang and Suslov, Dmitry and Stützer, Robert and Hardi, Justin and Oschwald, Michael (2022) Flame Characteristics and Response of a High-Pressure LOX/CNG Rocket Combustor with Large Optical Access. Aerospace. Multidisciplinary Digital Publishing Institute (MDPI). doi: 10.3390/aerospace9080410. ISSN 2226-4310.

[img] PDF - Published version
1MB

Official URL: https://www.mdpi.com/2226-4310/9/8/410


Item URL in elib:https://elib.dlr.de/191714/
Document Type:Article
Title:Flame Characteristics and Response of a High-Pressure LOX/CNG Rocket Combustor with Large Optical Access
Authors:
AuthorsInstitution or Email of AuthorsAuthor's ORCID iDORCID Put Code
Martin, JanUNSPECIFIEDhttps://orcid.org/0000-0002-5050-2506UNSPECIFIED
Armbruster, WolfgangUNSPECIFIEDhttps://orcid.org/0000-0002-4859-4173UNSPECIFIED
Suslov, DmitryUNSPECIFIEDhttps://orcid.org/0000-0002-5160-9292UNSPECIFIED
Stützer, RobertUNSPECIFIEDhttps://orcid.org/0000-0003-4136-8496UNSPECIFIED
Hardi, JustinUNSPECIFIEDhttps://orcid.org/0000-0003-3258-5261UNSPECIFIED
Oschwald, MichaelUNSPECIFIEDhttps://orcid.org/0000-0002-9579-9825UNSPECIFIED
Date:2022
Journal or Publication Title:Aerospace
Refereed publication:Yes
Open Access:Yes
Gold Open Access:Yes
In SCOPUS:Yes
In ISI Web of Science:Yes
DOI:10.3390/aerospace9080410
Publisher:Multidisciplinary Digital Publishing Institute (MDPI)
ISSN:2226-4310
Status:Published
Keywords:liquid propellant rocket engine; supercritical combustion; optical access; LOX/Methane; single-injector
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: Lampoldshausen
Institutes and Institutions:Institute of Space Propulsion > Rocket Propulsion Technology
Institute of Space Propulsion > Rocket Engine Systems
Institute of Space Propulsion > Leitungsbereich RA
Deposited By: Hanke, Michaela
Deposited On:13 Dec 2022 07:52
Last Modified:13 Dec 2022 07:52

Repository Staff Only: item control page

Browse
Search
Help & Contact
Information
OpenAIRE Validator logo electronic library is running on EPrints 3.3.12
Website and database design: Copyright © German Aerospace Center (DLR). All rights reserved.