Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 130
Book Description
Aerothermodynamic Assessment of Corrugated Panel Thermal Protection Systems
Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 130
Book Description
Publisher:
ISBN:
Category :
Languages : en
Pages : 130
Book Description
Scientific and Technical Aerospace Reports
Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 1018
Book Description
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 1018
Book Description
NASA Technical Paper
Author:
Publisher:
ISBN:
Category : Science
Languages : en
Pages : 52
Book Description
Publisher:
ISBN:
Category : Science
Languages : en
Pages : 52
Book Description
Scientific and Technical Aerospace Reports
Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 1294
Book Description
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 1294
Book Description
Aerodynamic Heating on the Corrugated Surface of a 10.20 Half-angle Blunted Cone at Mach 6.7
Author: Irving Weinstein
Publisher:
ISBN:
Category : Cone
Languages : en
Pages : 50
Book Description
Publisher:
ISBN:
Category : Cone
Languages : en
Pages : 50
Book Description
International Aerospace Abstracts
Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 974
Book Description
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 974
Book Description
Astronautics & Aeronautics
Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 812
Book Description
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 812
Book Description
Aerothermodynamics and Thermal Control Analysis for the Heat Sink Thermal Protection System of a Flyback Booster
Author: Gregory R. Jones
Publisher:
ISBN:
Category :
Languages : en
Pages :
Book Description
Publisher:
ISBN:
Category :
Languages : en
Pages :
Book Description
Heart Aerothermodynamic Analysis
Author: Alireza Mazaheri
Publisher: BiblioGov
ISBN: 9781289168667
Category :
Languages : en
Pages : 38
Book Description
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.
Publisher: BiblioGov
ISBN: 9781289168667
Category :
Languages : en
Pages : 38
Book Description
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.
Evaluation of Three Thermal Protection Systems in a Hypersonic High-heating-rate Environment Induces by an Elevon Deflected 30/̊
Author: Allan H. Taylor
Publisher:
ISBN:
Category : Insulating materials
Languages : en
Pages : 42
Book Description
Publisher:
ISBN:
Category : Insulating materials
Languages : en
Pages : 42
Book Description