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Cryogenic Propellant Tank and Feedline Design Studies in the Framework of the CHATT Project

Schwanekamp, Tobias and Ludwig, Carina and Sippel, Martin (2014) Cryogenic Propellant Tank and Feedline Design Studies in the Framework of the CHATT Project. In: AIAA AVIATION 2014 -19th AIAA International Space Planes and Hypersonic Systems and Technologies Conference 2014. Deutsches Zentrum für Luft- und Raumfahrt (DLR). 19th AIAA International Space Planes and Hypersonic Systems and Technologies Conference, 2014-06-16 - 2014-06-20, Atlanta, GA, USA. doi: 10.2514/6.2014-2370.

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Abstract

The EU-funded project CHATT (Cryogenic Hypersonic Advanced Tank Technologies) has been initiated early 2012 and is part of the European Commission’s Seventh Framework Programme (FP7). CHATT focuses on the development of novel cryogenic tank and propellant supply technologies. One of the tasks within the project is the investigation of adequate propellant crossfeed systems. Propellant crossfeed principally allows large mass savings for parallel burn vehicles such as the visionary passenger transport concept “SpaceLiner” which has been proposed by the Space Launcher Systems Analysis Department of the German Aerospace Center DLR. Therefore the tank and feedline systems of the SpaceLiner concept are studied by means of reference data and the results of simulations conducted with in-house and commercial tools.

Item URL in elib:https://elib.dlr.de/89861/
Document Type:Conference or Workshop Item (Speech)
Title:Cryogenic Propellant Tank and Feedline Design Studies in the Framework of the CHATT Project
Authors:
AuthorsInstitution or Email of AuthorsAuthor's ORCID iDORCID Put Code
Schwanekamp, TobiasUNSPECIFIEDUNSPECIFIEDUNSPECIFIED
Ludwig, CarinaUNSPECIFIEDUNSPECIFIEDUNSPECIFIED
Sippel, MartinUNSPECIFIEDhttps://orcid.org/0000-0001-7356-7575UNSPECIFIED
Date:June 2014
Journal or Publication Title:AIAA AVIATION 2014 -19th AIAA International Space Planes and Hypersonic Systems and Technologies Conference 2014
Refereed publication:No
Open Access:Yes
Gold Open Access:No
In SCOPUS:Yes
In ISI Web of Science:No
DOI:10.2514/6.2014-2370
Editors:
EditorsEmailEditor's ORCID iDORCID Put Code
Schwanekamp, TobiasUNSPECIFIEDUNSPECIFIEDUNSPECIFIED
Ludwig, CarinaUNSPECIFIEDUNSPECIFIEDUNSPECIFIED
Sippel, MartinUNSPECIFIEDUNSPECIFIEDUNSPECIFIED
Publisher:Deutsches Zentrum für Luft- und Raumfahrt (DLR)
Series Name:AIAA
Status:Published
Keywords:Propellant Crossfeed, Feedline Design, Cryogenic Tanks, SpaceLiner, High Speed Passenger Transport, Hypersonic Flight
Event Title:19th AIAA International Space Planes and Hypersonic Systems and Technologies Conference
Event Location:Atlanta, GA, USA
Event Type:international Conference
Event Start Date:16 June 2014
Event End Date:20 June 2014
Organizer:AIAA
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 - Raumfahrzeugsysteme - Systemanalyse Raumtransport (old)
Location: Bremen
Institutes and Institutions:Institute of Space Systems > Space Launcher Systems Analysis
Deposited By: Schwanekamp, Tobias
Deposited On:22 Jul 2014 12:26
Last Modified:24 Apr 2024 19:55

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