elib
DLR-Header
DLR-Logo -> http://www.dlr.de
DLR Portal Home | Impressum | Datenschutz | Barrierefreiheit | Kontakt | English
Schriftgröße: [-] Text [+]

Development of cryogenic tanks using the Scaled Half-Tank Test

Liebisch, Martin und Rehra, Jan und Wille, Tobias (2026) Development of cryogenic tanks using the Scaled Half-Tank Test. DLRK 2026, 2026-09-08 - 2026-09-10, Aachen.

[img] PDF - Nur DLR-intern zugänglich
3MB
[img] PDF - Nur DLR-intern zugänglich
526kB

Kurzfassung

Liquid hydrogen (LH₂) storage tanks made from carbon fibre-reinforced polymers (CFRP) offer significant advantages for aerospace applications but at the same time require profound understanding of their thermomechanical behaviour at cryogenic temperatures down to ~20 K. Current validation strategies remain fragmented between material-level coupon testing and full-scale tank validation, leaving a critical gap for intermediate-scale structural assessment. This paper presents a Scaled Half-Tank Test methodology utilizing a 400 mm diameter CFRP specimen to bridge this gap. The experimental test rig features a pressure vessel recipient that isolates internal and external volumes, enabling independent control of thermal gradients and differential pressure. Comprehensive instrumentation, including strain sensors, thermocouples, and optical windows, allows real-time correlation of thermomechanical deformation with permeation behavior. The evaluation strategy employs iterative pressurization under stationary thermal states at ambient and cryogenic conditions. Diffusive transport is characterized through asymptotic leak rate plateaus while damage related onset of leakage is captured by abrupt leak rate increase. The test concept, subsystem functionality and expected permeation profiles are successfully validated by initial tests. Ongoing studies are focusing on detailed assessment of tank sealings, cryogenic sensor sensitivities, and correlation of integral system data with local material models.

elib-URL des Eintrags:https://elib.dlr.de/226868/
Dokumentart:Konferenzbeitrag (Vortrag)
Zusätzliche Informationen:This research was funded by the German funded UpLift-Project, FKZ 20M2268. https://www.uplift-h2-aviation.de/uplift/ The CONCERTO project is supported by the Clean Aviation Joint Undertaking and its members. Funded by the European Union, under Grant Agreement No 101101999. Views and opinions expressed are however those of the author(s) only and do not necessarily reflect those of the European Union or Clean Aviation Joint Undertaking. Neither the European Union nor Clean Aviation JU can be held responsible for them
Titel:Development of cryogenic tanks using the Scaled Half-Tank Test
Autoren:
AutorenInstitution oder E-Mail-AdresseAutoren-ORCID-iDORCID Put Code
Liebisch, MartinMartin.Liebisch (at) dlr.dehttps://orcid.org/0000-0001-5423-7511NICHT SPEZIFIZIERT
Rehra, Janjan.rehra (at) dlr.deNICHT SPEZIFIZIERTNICHT SPEZIFIZIERT
Wille, TobiasTobias.Wille (at) dlr.dehttps://orcid.org/0009-0009-5777-2822NICHT SPEZIFIZIERT
Datum:2026
Referierte Publikation:Ja
Open Access:Nein
Gold Open Access:Nein
In SCOPUS:Nein
In ISI Web of Science:Nein
Status:akzeptierter Beitrag
Stichwörter:Liquid hydrogen, LH2, Cryogenic testing, Tanks
Veranstaltungstitel:DLRK 2026
Veranstaltungsort:Aachen
Veranstaltungsart:nationale Konferenz
Veranstaltungsbeginn:8 September 2026
Veranstaltungsende:10 September 2026
HGF - Forschungsbereich:Luftfahrt, Raumfahrt und Verkehr
HGF - Programm:Luftfahrt
HGF - Programmthema:Komponenten und Systeme
DLR - Schwerpunkt:Luftfahrt
DLR - Forschungsgebiet:L CS - Komponenten und Systeme
DLR - Teilgebiet (Projekt, Vorhaben):L - Strukturwerkstoffe und Bauweisen
Standort: Braunschweig
Institute & Einrichtungen:Institut für Systemleichtbau > Strukturmechanik
Hinterlegt von: Liebisch, Martin
Hinterlegt am:30 Sep 2026 19:45
Letzte Änderung:02 Okt 2026 11:07

Nur für Mitarbeiter des Archivs: Kontrollseite des Eintrags

Blättern
Suchen
Hilfe & Kontakt
Informationen
OpenAIRE Validator logo electronic library verwendet EPrints
Gestaltung Webseite und Datenbank: Copyright © Deutsches Zentrum für Luft- und Raumfahrt (DLR). Alle Rechte vorbehalten.