Garbers, Nicole (2014) Metallic Thermal Protection System for SpaceLiner. DLR-Interner Bericht. SART TN-016/2014. Other. DLR. (Unpublished)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/ | ||||||||
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Document Type: | Monograph (DLR-Interner Bericht, Other) | ||||||||
Additional Information: | .pdf auf Anfrage bei RY-SRT erhältlich! | ||||||||
Title: | Metallic Thermal Protection System for SpaceLiner | ||||||||
Authors: |
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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Status: | Unpublished | ||||||||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 Transportation | ||||||||
DLR - Research area: | Raumfahrt | ||||||||
DLR - Program: | R RP - Space Transportation | ||||||||
DLR - Research theme (Project): | R - Raumfahrzeugsysteme - Systemanalyse Raumtransport (old) | ||||||||
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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