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Technical Progress of Multiple-Mission Reusable Launch Vehicle SpaceLiner

Sippel, Martin and Stappert, Sven and Bussler, Leonid and Forbes-Spyratos, Sholto (2018) Technical Progress of Multiple-Mission Reusable Launch Vehicle SpaceLiner. HiSST 2018, 26–29 November 2018, Moskau, Russland.

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Abstract

The SpaceLiner ultra-high-speed rocket-propelled passenger transport is in Phase A conceptual design after successful completion of the MRR. The ongoing concept evolution is addressing system aspects of the next configuration release 8. The space transportation role of the SpaceLiner concept as a TSTO-launcher is further refined and suitable precursor steps are investigated. The critical separation of the passenger cabin and rescue capsule and its subsystems are one topic of the paper. The separation process is critically investigated taking into account multi-body dynamics and advanced CFD-simulations. Potential intercontinental flight routes, considering range-safety and sonic boom constraints as well as good reachability from major business centers, are evaluated Extensions to this trajectory model are implemented to investigate the attitude dynamics and related controllability issues of the asymmetric launcher configuration.

Item URL in elib:https://elib.dlr.de/125919/
Document Type:Conference or Workshop Item (Speech)
Additional Information:Dokumentennummer: HiSST 2018-1580839
Title:Technical Progress of Multiple-Mission Reusable Launch Vehicle SpaceLiner
Authors:
AuthorsInstitution or Email of AuthorsAuthors ORCID iD
Sippel, Martinmartin.sippel (at) dlr.dehttps://orcid.org/0000-0001-7356-7575
Stappert, SvenSven.Stappert (at) dlr.dehttps://orcid.org/0000-0002-8425-2779
Bussler, Leonidleonid.bussler (at) dlr.dehttps://orcid.org/0000-0002-0657-4086
Forbes-Spyratos, SholtoUniversity of Queensland, BrisbaneUNSPECIFIED
Date:2018
Refereed publication:No
Open Access:Yes
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:No
Status:Published
Keywords:SpaceLiner, RLV, SLME, multi body simulation, trajectory simulation
Event Title:HiSST 2018
Event Location:Moskau, Russland
Event Type:international Conference
Event Dates:26–29 November 2018
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 > Space Launcher Systems Analysis
Deposited By: Vormschlag, Nele Marei
Deposited On:16 Jan 2019 09:46
Last Modified:31 Jul 2019 20:23

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