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Metallic Thermal Protection System for SpaceLiner

Garbers, Nicole (2014) Metallic Thermal Protection System for SpaceLiner. DLR-Forschungsbericht. SART TN-16/2014. (Unpublished)

Full text not available from this repository.

Abstract

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/91915/
Document Type:Monograph (DLR-Forschungsbericht)
Title:Metallic Thermal Protection System for SpaceLiner
Authors:
AuthorsInstitution or Email of AuthorsAuthors ORCID iD
Garbers, NicoleUNSPECIFIEDUNSPECIFIED
Date: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Status:Unpublished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 Bremen
Department:SART
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: Behnke, Manuela
Deposited On:27 Nov 2014 10:40
Last Modified:27 Nov 2014 10:40

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