Free-flight Investigation of Ablation Effects N the Stability of Conical Reentry Configurations

Free-flight Investigation of Ablation Effects N the Stability of Conical Reentry Configurations PDF Author: C. J. Welsh
Publisher:
ISBN:
Category : Ablation (Aerothermodynamics)
Languages : en
Pages : 40

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Book Description
A 1000-ft aeroballistics range was used to obtain free-flight stability and drag data for slightly blunted 10-deg semiangle cones with and without ablation occurring on the conical skirts. The configurations investigated included ones having fore- and aft-positioned ablation sleeves, as well as one with a skirt material which did not ablate. The investigation was conducted for a Mach number near 14 and a Reynolds number, based on cone length and free-stream conditions, of about 55000.

Free-flight Investigation of Ablation Effects N the Stability of Conical Reentry Configurations

Free-flight Investigation of Ablation Effects N the Stability of Conical Reentry Configurations PDF Author: C. J. Welsh
Publisher:
ISBN:
Category : Ablation (Aerothermodynamics)
Languages : en
Pages : 40

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Book Description
A 1000-ft aeroballistics range was used to obtain free-flight stability and drag data for slightly blunted 10-deg semiangle cones with and without ablation occurring on the conical skirts. The configurations investigated included ones having fore- and aft-positioned ablation sleeves, as well as one with a skirt material which did not ablate. The investigation was conducted for a Mach number near 14 and a Reynolds number, based on cone length and free-stream conditions, of about 55000.

Free-Flight Investigation of Ablation Effects on the Stability of Conical Reentry Configurations

Free-Flight Investigation of Ablation Effects on the Stability of Conical Reentry Configurations PDF Author: C. J. Welsh
Publisher:
ISBN:
Category :
Languages : en
Pages : 33

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Book Description
A 1000-ft aeroballistics range was used to obtain free-flight stability and drag data for slightly blunted 10-deg semiangle cones with and without ablation occurring on the conical skirts. The configurations investigated included ones having fore- and aft-positioned ablation sleeves, as well as one with a skirt material which did not ablate. The investigation was conducted for a Mach number near 14 and a Reynolds number, based on cone length and free-stream conditions, of about 55000.

Free-flight Investigation of Ablation Effects N the Stability of Conical Reentry Configurations

Free-flight Investigation of Ablation Effects N the Stability of Conical Reentry Configurations PDF Author: C. J. Welsh
Publisher:
ISBN:
Category : Ablation (Aerothermodynamics).
Languages : en
Pages : 0

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Book Description
A 1000-ft aeroballistics range was used to obtain free-flight stability and drag data for slightly blunted 10-deg semiangle cones with and without ablation occurring on the conical skirts. The configurations investigated included ones having fore- and aft-positioned ablation sleeves, as well as one with a skirt material which did not ablate. The investigation was conducted for a Mach number near 14 and a Reynolds number, based on cone length and free-stream conditions, of about 55000.

Scientific and Technical Aerospace Reports

Scientific and Technical Aerospace Reports PDF Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 978

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Aerodynamic Testing in a Free-flight Spark Range

Aerodynamic Testing in a Free-flight Spark Range PDF Author: G. L. Winchenbach
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ISBN:
Category : Aerodynamics
Languages : en
Pages : 172

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Real-gas Effects on the Aerodynamics of Blunt Cones as Measured in a Hypervelocity Range

Real-gas Effects on the Aerodynamics of Blunt Cones as Measured in a Hypervelocity Range PDF Author: C. J. Welsh
Publisher:
ISBN:
Category : Aerodynamics, Hypersonic
Languages : en
Pages : 32

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Investigation of Ablation Effects on Hypersonic Dynamic Stability of a 10 Degrees Cone

Investigation of Ablation Effects on Hypersonic Dynamic Stability of a 10 Degrees Cone PDF Author: Dave R. Moore
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Category :
Languages : en
Pages : 84

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NASA Scientific and Technical Reports

NASA Scientific and Technical Reports PDF Author: United States. National Aeronautics and Space Administration Scientific and Technical Information Division
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 1440

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Technical Abstract Bulletin

Technical Abstract Bulletin PDF Author:
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ISBN:
Category : Science
Languages : en
Pages : 628

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A Selected Listing of NASA Scientific and Technical Reports for ...

A Selected Listing of NASA Scientific and Technical Reports for ... PDF Author: United States. National Aeronautics and Space Administration. Scientific and Technical Information Division
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 1680

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