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STRUCTURAL AND TPS TRADE-OFF STUDIES AND DESIGN OPTIONS FOR THE HYPERSONIC TRANSPORT SYSTEM SPACELINER

Kopp, Alexander and Garbers, Nicole (2014) STRUCTURAL AND TPS TRADE-OFF STUDIES AND DESIGN OPTIONS FOR THE HYPERSONIC TRANSPORT SYSTEM SPACELINER. European Conference on Spacecraft Structures, Materials & Environmental Testing, 01.-04.04.2014, Braunschweig, Deutschland. (Unpublished)

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Abstract

The SpaceLiner is a rocket propelled, hypersonic transport aircraft concept, with its launch being assisted by a separate booster stage. This paper presents structural trade-off investigations for the SpaceLiner. Structural materials, structural concepts and member spacing will be compared, and the results discussed. The impact of minimum gauge thickness and TPS integration will be investigated as well. The analysis methodology will be described. Furthermore, the integration of the passenger rescue stage into the vehicle structure will be addressed, with initial results being shown.

Document Type:Conference or Workshop Item (Speech)
Title:STRUCTURAL AND TPS TRADE-OFF STUDIES AND DESIGN OPTIONS FOR THE HYPERSONIC TRANSPORT SYSTEM SPACELINER
Authors:
AuthorsInstitution or Email of Authors
Kopp, Alexanderalexander.kopp@dlr.de
Garbers, Nicolenicole.garbers@dlr.de
Date:April 2014
Refereed publication:No
Status:Unpublished
Keywords:SpaceLiner, Structure, TPS, Optimization
Event Title:European Conference on Spacecraft Structures, Materials & Environmental Testing
Event Location:Braunschweig, Deutschland
Event Type:international Conference
Event Dates:01.-04.04.2014
Organizer:ESA,DLR,CNES
HGF - Research field:Aeronautics, Space and Transport
HGF - Program:Space
HGF - Program Themes:Space Transport
DLR - Research area:Raumfahrt
DLR - Program:R RP - Raumtransport
DLR - Research theme (Project):R - Raumfahrzeugsysteme - Systemanalyse Raumtransport
Location: Bremen
Institutes and Institutions:Institute of Space Systems > Systemanalyse Raumtransport
Deposited By: Manuela Behnke
Deposited On:29 Apr 2014 10:41
Last Modified:08 May 2014 23:21

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