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System Studies on Active Thermal Protection of a Hypersonic Suborbital Passenger Transport Vehicle

Schwanekamp, Tobias and Meyer, Frank and Reimer, Thomas and Petkov, Ivaylo and Tröltzsch, Anke and Siggel, Martin (2014) System Studies on Active Thermal Protection of a Hypersonic Suborbital Passenger Transport Vehicle. In: 19th AIAA International Space Planes and Hypersonic Systems and Technologies Conference. AIAA. 19th AIAA International Space Planes and Hypersonic Systems and Technologies Conference, 16.-20. Juni 2014, Atlanta, GA, USA.

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Abstract

Aerodynamic heating is a critical design aspect for the development of reusable hypersonic transport and reentry vehicles. The reliability in terms of thermal resistance is one of the major driving factors with respect to the design margins, the mass balance and finally the total costs of a configuration. Potential designs of active cooling systems for critical regions such as the vehicle nose and leading edges are presented as well as preliminary approaches for their impact on the total mass. The visionary suborbital passenger transport concept SpaceLiner is taken as a reference vehicle for these studies. Covering the whole flight regime from subsonic to Mach numbers of more than 20, this vehicle creates high demands on the thermal protection system. Part of the work was performed within the DLR research project THERMAS.

Item URL in elib:https://elib.dlr.de/92953/
Document Type:Conference or Workshop Item (Speech)
Title:System Studies on Active Thermal Protection of a Hypersonic Suborbital Passenger Transport Vehicle
Authors:
AuthorsInstitution or Email of AuthorsAuthors ORCID iD
Schwanekamp, TobiasTobias.Schwanekamp (at) dlr.deUNSPECIFIED
Meyer, FrankUNSPECIFIEDUNSPECIFIED
Reimer, Thomasthomas.reimer (at) dlr.deUNSPECIFIED
Petkov, IvayloIvaylo.Petkov (at) dlr.deUNSPECIFIED
Tröltzsch, Ankeanke.troeltzsch (at) dlr.deUNSPECIFIED
Siggel, Martinmartin.siggel (at) dlr.deUNSPECIFIED
Date:June 2014
Journal or Publication Title:19th AIAA International Space Planes and Hypersonic Systems and Technologies Conference
Refereed publication:No
Open Access:Yes
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:No
Editors:
EditorsEmail
Schwanekamp, TobiasUNSPECIFIED
Meyer, FrankUNSPECIFIED
Reimer, ThomasUNSPECIFIED
Petkov, IvayloUNSPECIFIED
Tröltzsch, AnkeUNSPECIFIED
Publisher:AIAA
Status:Published
Keywords:Thermal Protection System, Active Cooling, Hypersonic Passenger Transport, Aerodynamic Heating, SpaceLiner
Event Title:19th AIAA International Space Planes and Hypersonic Systems and Technologies Conference
Event Location:Atlanta, GA, USA
Event Type:international Conference
Event Dates:16.-20. Juni 2014
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, R - Proj. Thermas (old)
Location: Stuttgart
Institutes and Institutions:Institute of Space Systems > Space Launcher Systems Analysis
Institute of Structures and Design
Institut of Simulation and Software Technology
Institut of Simulation and Software Technology > Distributed Systems and Component Software
Deposited By: Schwanekamp, Tobias
Deposited On:09 Dec 2014 14:27
Last Modified:31 Jul 2019 19:50

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