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SpaceLiner Technical Progress and Mission Definition

Sippel, Martin and Schwanekamp, Tobias and Trivailo, Olga and Kopp, Alexander and Bauer, Carola and Garbers, Nicole (2015) SpaceLiner Technical Progress and Mission Definition. In: AIAA 2015-3582 (3582). AIAA. 20th AIAA International Space Planes and Hypersonic Systems and Technologies Conference, 6-9 July 2015, Glasgow, United Kingdom. DOI: 10.2514/6.2015-3582

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Official URL: http://arc.aiaa.org/doi/abs/10.2514/6.2015-3582

Abstract

DLR’s launcher systems analysis division is investigating since a couple of years a visionary, extremely fast passenger transportation concept reaching the edges of space based on rocket propulsion. Thanks to multi-national collaboration, the technical lay-out of the SpaceLiner has now matured to Phase A conceptual design level. Iterative sizing of all major subcomponents in nominal and off-nominal flight conditions has been performed. The paper describes the recent technical progress achieved in the SpaceLiner 7 configuration, • mainly system aspects of the reference vehicle’s preliminary design including establishment of a preliminary structural concept, • main propulsion system definition, • pre-development of a passenger cabin and rescue capsule and its specific challenges, • preliminary sizing of the thermal protection and active cooling systems, • mission definition with its nominal trajectories including potential ground infrastructure, • programmatic development aspects

Item URL in elib:https://elib.dlr.de/101481/
Document Type:Conference or Workshop Item (Speech)
Title:SpaceLiner Technical Progress and Mission Definition
Authors:
AuthorsInstitution or Email of AuthorsAuthors ORCID iD
Sippel, Martinmartin.sippel (at) dlr.dehttps://orcid.org/0000-0001-7356-7575
Schwanekamp, TobiasDLRUNSPECIFIED
Trivailo, OlgaOlga.Trivailo (at) dlr.deUNSPECIFIED
Kopp, Alexanderalexander.kopp (at) dlr.deUNSPECIFIED
Bauer, CarolaDLRUNSPECIFIED
Garbers, Nicolenicole.garbers (at) dlr.deUNSPECIFIED
Date:6 July 2015
Journal or Publication Title:AIAA 2015-3582
Refereed publication:Yes
Open Access:Yes
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:No
DOI :10.2514/6.2015-3582
Publisher:AIAA
Series Name:AIAA 2015-3582
Status:Published
Keywords:SpaceLiner, RLV, preliminary structural concept, thermal protection, active cooling systems, nominal trajectories
Event Title:20th AIAA International Space Planes and Hypersonic Systems and Technologies Conference
Event Location:Glasgow, United Kingdom
Event Type:international Conference
Event Dates:6-9 July 2015
Organizer:AIAA
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
Deposited By: Vormschlag, Nele Marei
Deposited On:14 Jan 2016 12:07
Last Modified:31 Jul 2019 19:59

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