Aerothermodynamic Assessment of Corrugated Panel Thermal Protection Systems PDF Download
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Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 130
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Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 130
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Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 1018
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Author:
Publisher:
ISBN:
Category : Science
Languages : en
Pages : 52
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Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 1294
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Author: Irving Weinstein
Publisher:
ISBN:
Category : Cone
Languages : en
Pages : 50
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Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 974
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Author:
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ISBN:
Category : Aeronautics
Languages : en
Pages : 812
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Author: Gregory R. Jones
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Category :
Languages : en
Pages :
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Author: Alireza Mazaheri
Publisher: BiblioGov
ISBN: 9781289168667
Category :
Languages : en
Pages : 38
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This paper presents an assessment of the aerothermodynamic environment around an 8.3 meter High Energy Atmospheric Reentry Test (HEART) vehicle. This study generated twelve nose shape configurations and compared their responses at the peak heating trajectory point against the baseline nose shape. The heat flux sensitivity to the angle of attack variations are also discussed. The possibility of a two-piece Thermal Protection System (TPS) design at the nose is also considered, as are the surface catalytic affects of the aeroheating environment of such configuration. Based on these analyses, an optimum nose shape is proposed to minimize the surface heating. A recommendation is also made for a two-piece TPS design, for which the surface catalytic uncertainty associated with the jump in heating at the nose-IAD juncture is reduced by a minimum of 93%. In this paper, the aeroshell is assumed to be rigid and the inflatable fluid interaction effect is left for future investigations.
Author: Allan H. Taylor
Publisher:
ISBN:
Category : Insulating materials
Languages : en
Pages : 42
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