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Metallic Thermal Protection System for SpaceLiner

Garbers, Nicole (2014) Metallic Thermal Protection System for SpaceLiner. Other. DLR-Interner Bericht. SART TN-016/2014. (Unpublished)

Full text not available from this repository.

Abstract

Until now, the SpaceLiner TPS uses mainly SpaceShuttle TPS materials. In this report, a metallic thermal protection system is considered for the temperature range between 900 – 1400 K.

Item URL in elib:https://elib.dlr.de/111435/
Document Type:Monograph (DLR-Interner Bericht, Other)
Additional Information:.pdf auf Anfrage bei RY-SRT erhältlich!
Title:Metallic Thermal Protection System for SpaceLiner
Authors:
AuthorsInstitution or Email of AuthorsAuthors ORCID iD
Garbers, Nicolenicole.garbers (at) dlr.deUNSPECIFIED
Date:19 August 2014
Refereed publication:No
Open Access:No
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:No
Status:Unpublished
Keywords:TPS, SpaceLiner, metallic, Internal Flexible Insulation
Institution:DLR
Department:RY-SRT
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:09 Mar 2017 09:59
Last Modified:09 Mar 2017 09:59

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