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Flame Characteristics 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 of a High-Pressure LOX/CNG Rocket Combustor with Large Optical Access. In: 33rd International Symposium on Space Technology and Science. 33rd International Symposium on Space Technology and Science, 2022-02-26 - 2022-03-04, Oita, Japan.

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Official URL: https://confit.atlas.jp/guide/event/ists2021/subject/A-4-05/advanced


Item URL in elib:https://elib.dlr.de/191599/
Document Type:Conference or Workshop Item (Speech)
Title:Flame Characteristics 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:33rd International Symposium on Space Technology and Science
Refereed publication:Yes
Open Access:No
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:No
Status:Published
Keywords:rocket engine, sub-/supercritical combustion, optical access, liquid oxygen / compressed natural gas, single-injector
Event Title:33rd International Symposium on Space Technology and Science
Event Location:Oita, Japan
Event Type:international Conference
Event Start Date:26 February 2022
Event End Date:4 March 2022
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:05 Dec 2022 15:48
Last Modified:24 Apr 2024 20:52

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