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INVESTIGATION OF THE ASCENT FLIGHT DYNAMICS OF THE SPACELINER CONCEPT AS A NON-SYMMETRIC LAUNCHER CONFIGURATION

Krummen, Sven and Sippel, Martin (2017) INVESTIGATION OF THE ASCENT FLIGHT DYNAMICS OF THE SPACELINER CONCEPT AS A NON-SYMMETRIC LAUNCHER CONFIGURATION. Deutscher Luft- und Raumfahrtkongress 2017, 5.-.7. September 2017, München, Deutschland.

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Official URL: http://www.dlrk2017.dglr.de/nc/paper_download/index.html

Abstract

Determining the flight dynamic characteristics of a space transportation vehicle in its preliminary design phase is a complex task since a large variety of vehicle parameters need to be estimated. For the SpaceLiner vehicle, a concept of a hypersonic suborbital space plane, such an analysis has now been established. In this study a 6 DOF trajectory simulation has been developed to assess the general feasibility of fulfilling the mission requirements during nominal and off-nominal flight conditions.

Item URL in elib:https://elib.dlr.de/114996/
Document Type:Conference or Workshop Item (Speech)
Title:INVESTIGATION OF THE ASCENT FLIGHT DYNAMICS OF THE SPACELINER CONCEPT AS A NON-SYMMETRIC LAUNCHER CONFIGURATION
Authors:
AuthorsInstitution or Email of AuthorsAuthors ORCID iD
Krummen, Svensven.krummen (at) dlr.deUNSPECIFIED
Sippel, MartinMartin.Sippel (at) dlr.dehttps://orcid.org/0000-0001-7356-7575
Date:2017
Refereed publication:No
Open Access:Yes
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:No
Status:Published
Keywords:SpaceLiner, Flight Dynamics, Thrust Vector Control, TRACE, 6 DOF, Trajectory Simulation, Relay Autotuning, Trimmability
Event Title:Deutscher Luft- und Raumfahrtkongress 2017
Event Location:München, Deutschland
Event Type:national Conference
Event Dates:5.-.7. September 2017
Organizer:DGLR
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:08 Nov 2017 08:58
Last Modified:31 Jul 2019 20:12

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