elib
DLR-Header
DLR-Logo -> http://www.dlr.de
DLR Portal Home | Imprint | Privacy Policy | Contact | Deutsch
Fontsize: [-] Text [+]

Advanced Simulations of Reusable Hypersonic Rocket-Powered Stages

Sippel, Martin and Bussler, Leonid and Kopp, Alexander and Krummen, Sven and Valluchi, Cecilia and Wilken, Jascha (2017) Advanced Simulations of Reusable Hypersonic Rocket-Powered Stages. 21st AIAA International Space Planes and Hypersonics Technologies Conference, 6-9 March 2017, Xiamen, China. DOI: 10.2514/6.2017-2170

[img] PDF
2MB

Official URL: https://arc.aiaa.org/doi/pdf/10.2514/6.2017-2170

Abstract

After successful completion of the MRR, technical progress of the SpaceLiner ultra-high-speed rocket-propelled passenger transport is achieved in Phase A conceptual design work. Following geometry refinement the structural design is maturing based on extensive trade-offs. Aerodynamics are investigated by numerical CFD-simulations of the two winged stages and will be supported by windtunnel tests. Aerodynamic control surfaces of the passenger cabin and rescue capsule and its subsystems are defined. Alternative options for the capsule with innovative morphing shapes are critically investigated taking into account system aspects, structural design, 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 and flight guidance schemes are established. Extensions to this trajectory model are implemented to investigate the attitude dynamics and related controllability issues of the asymmetric launcher configuration. The space transportation role of the SpaceLiner concept as a TSTO-launcher is now addressed in technical detail.

Item URL in elib:https://elib.dlr.de/112472/
Document Type:Conference or Workshop Item (Speech)
Title:Advanced Simulations of Reusable Hypersonic Rocket-Powered Stages
Authors:
AuthorsInstitution or Email of AuthorsAuthors ORCID iD
Sippel, Martinmartin.sippel (at) dlr.dehttps://orcid.org/0000-0001-7356-7575
Bussler, Leonidleonid.bussler (at) dlr.deUNSPECIFIED
Kopp, AlexanderAlexander.Kopp (at) dlr.deUNSPECIFIED
Krummen, Svensven.krummen (at) dlr.deUNSPECIFIED
Valluchi, Ceciliacecilia.valluchi (at) dlr.deUNSPECIFIED
Wilken, Jaschajascha.wilken (at) dlr.dehttps://orcid.org/0000-0001-5748-1261
Date:2017
Refereed publication:No
Open Access:Yes
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:No
DOI :10.2514/6.2017-2170
Status:Published
Keywords:Spaceliner, RLV, capsule, CFD, structure design, trajectory simulation
Event Title:21st AIAA International Space Planes and Hypersonics Technologies Conference
Event Location:Xiamen, China
Event Type:international Conference
Event Dates:6-9 March 2017
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 > Space Launcher Systems Analysis
Deposited By: Vormschlag, Nele Marei
Deposited On:23 May 2017 09:34
Last Modified:31 Jul 2019 20:09

Repository Staff Only: item control page

Browse
Search
Help & Contact
Information
electronic library is running on EPrints 3.3.12
Copyright © 2008-2017 German Aerospace Center (DLR). All rights reserved.