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- W2334132642 abstract "With the SpaceLiner the DLR has proposed a visionary concept for hypersonic suborbital passenger transport over extremely long distances [1]. Depending on the configuration or mission type, the maximum flight Mach numbers of the vehicle can exceed Mach 20, hence the consideration of aerodynamic heating be-comes mandatory during the design process.The paper addresses the aerothermal challenges of the SpaceLiner flight and the latest updates in the conceptu-al design of the thermal protection system (TPS). Due to the very high heat loads, an active TPS is required for the nose and the leading edge whereas a passive, radia-tively cooled TPS is sufficient for the downstream sur-face regions. Potential solutions for both, active and passive thermal protection are developed and presented. Mass and systems requirements as well as an economi-cally justifiable effort for manufacturing and mainte-nance are constraints which are also taken into account during the whole design process." @default.
- W2334132642 created "2016-06-24" @default.
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- W2334132642 date "2015-03-01" @default.
- W2334132642 modified "2023-09-27" @default.
- W2334132642 title "CONCEPTUAL DESIGN OF THE SPACELINER THERMAL PROTECTION SYSTEM" @default.
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