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Cryogenic Hypersonic Advanced Tank Technologies Theme 7: TRANSPORT (including AERONAUTICS) Report Temperature Cycle Analysis

Fischer, Alexander (2015) Cryogenic Hypersonic Advanced Tank Technologies Theme 7: TRANSPORT (including AERONAUTICS) Report Temperature Cycle Analysis. Project Report. D4.3.1. (Unpublished)

Full text not available from this repository.

Abstract

The investigation in WP 4.3.2 is done on long term behaviour of CFRP structures and deals with the material properties of a potential propellant tank for rockets or hypersonic vehicles, which use liquid hydrogen (LH2) or Oxygen (LOX). The application of CFRP materials in tank structures for such cryogenic propellants is a demand for the verification of the material compatibility. Challenging is the application in a wide temperature range between ambient and very low temperatures (20 K for LH2 and 80 K for LOX respectively).

Item URL in elib:https://elib.dlr.de/100931/
Document Type:Monograph (Project Report)
Title:Cryogenic Hypersonic Advanced Tank Technologies Theme 7: TRANSPORT (including AERONAUTICS) Report Temperature Cycle Analysis
Authors:
AuthorsInstitution or Email of AuthorsAuthors ORCID iD
Fischer, AlexanderDLRUNSPECIFIED
Date:31 August 2015
Refereed publication:No
Open Access:No
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:No
Status:Unpublished
Keywords:CHATT, hypersonic vehicle, CFRP,
Institution:DLR Bremen
Department:TAS
HGF - Research field:Aeronautics, Space and Transport
HGF - Program:Space
HGF - Program Themes:other
DLR - Research area:Raumfahrt
DLR - Program:R - no assignment
DLR - Research theme (Project):R - no assignment
Location: Bremen
Institutes and Institutions:Institute of Space Systems > Transport and Propulsion System
Deposited By: Behnke, Manuela
Deposited On:21 Jan 2016 09:23
Last Modified:10 May 2016 23:38

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