Static aerodynamic characteristics of a 1/9- scale model of the escape and exit configurations of the Project Mercury spacecraft at Mach numbers from 2.30 to 4.65 PDF Download

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Static aerodynamic characteristics of a 1/9- scale model of the escape and exit configurations of the Project Mercury spacecraft at Mach numbers from 2.30 to 4.65

Static aerodynamic characteristics of a 1/9- scale model of the escape and exit configurations of the Project Mercury spacecraft at Mach numbers from 2.30 to 4.65 PDF Author: R. H. Fournier
Publisher:
ISBN:
Category : Technology & Engineering
Languages : en
Pages : 27

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Book Description

Static aerodynamic characteristics of a 1/9- scale model of the escape and exit configurations of the Project Mercury spacecraft at Mach numbers from 2.30 to 4.65

Static aerodynamic characteristics of a 1/9- scale model of the escape and exit configurations of the Project Mercury spacecraft at Mach numbers from 2.30 to 4.65 PDF Author: R. H. Fournier
Publisher:
ISBN:
Category : Technology & Engineering
Languages : en
Pages : 27

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Book Description

Wind-tunnel Investigation of Static Aerodynamic Characteristics of a 1/9-scale Model of a Project Mercury Capsule at Mach Numbers from 1.60 to 4.65

Wind-tunnel Investigation of Static Aerodynamic Characteristics of a 1/9-scale Model of a Project Mercury Capsule at Mach Numbers from 1.60 to 4.65 PDF Author: David S. Shaw
Publisher:
ISBN:
Category : Space vehicles
Languages : en
Pages : 32

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Book Description

Wind-tunnel Investigation at Mach Numbers from 0.50 to 1.14 of the Static Aerodynamic Characteristics of a Model of a Project Mercury Capsule

Wind-tunnel Investigation at Mach Numbers from 0.50 to 1.14 of the Static Aerodynamic Characteristics of a Model of a Project Mercury Capsule PDF Author: Albin O. Pearson
Publisher:
ISBN:
Category : Space vehicles
Languages : en
Pages : 32

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Book Description

Wind-tunnel Investigation at Mach Numbers from 0.30 to 1.14 of the Static Aerodynamic Characteristics of Modified Mercury Escape and Exit Capsule Configurations

Wind-tunnel Investigation at Mach Numbers from 0.30 to 1.14 of the Static Aerodynamic Characteristics of Modified Mercury Escape and Exit Capsule Configurations PDF Author: Albin O. Pearson
Publisher:
ISBN:
Category : Noses (Space vehicles)
Languages : en
Pages : 40

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Book Description

Wind-tunnel Investigation of Static Aerodynamic Characteristics of a 1/9-scale Model of a Possible Reentry Capsule at Mach Numbers from 2.29 to 4.65

Wind-tunnel Investigation of Static Aerodynamic Characteristics of a 1/9-scale Model of a Possible Reentry Capsule at Mach Numbers from 2.29 to 4.65 PDF Author: David S. Shaw
Publisher:
ISBN:
Category : Space vehicles
Languages : en
Pages : 26

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Book Description

Static Longitudinal Stability Characteristics of Various Mercury Escape Configurations and of a Proposed Alternate Escape Configuration for Mach Numbers of 0.05 to 9.60

Static Longitudinal Stability Characteristics of Various Mercury Escape Configurations and of a Proposed Alternate Escape Configuration for Mach Numbers of 0.05 to 9.60 PDF Author: Robert P. Smith
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 186

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Book Description

Static Longitudinal Stability Characteristics of Various Mercury Escape Configurations and of a Proposed Alternate Escape Configuration for Mach Numbers of 0.05 to 9.60

Static Longitudinal Stability Characteristics of Various Mercury Escape Configurations and of a Proposed Alternate Escape Configuration for Mach Numbers of 0.05 to 9.60 PDF Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 184

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Book Description

Effects of Canted Forward Faces on the Static Longitudinal Stability Characteristics of the Escape and Exit Configurations of a Project Mercury Capsule Model at a Mach Number of 2.01

Effects of Canted Forward Faces on the Static Longitudinal Stability Characteristics of the Escape and Exit Configurations of a Project Mercury Capsule Model at a Mach Number of 2.01 PDF Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 20

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Book Description

Pressure Distribution on Two Models of a Project Mercury Capsule for a Mach Number Range of 1.60 to 6.01 and an Angle-of-attack Range of 0°degress to 180°

Pressure Distribution on Two Models of a Project Mercury Capsule for a Mach Number Range of 1.60 to 6.01 and an Angle-of-attack Range of 0°degress to 180° PDF Author: Robert A. Newlander
Publisher:
ISBN:
Category : Aerodynamic load
Languages : en
Pages : 100

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Book Description

Static Longitudinal Stability Characteristics of Various Mercury Escape Configurations and of a Proposed Alternate Escape Configuration for Mach Numbers of 0.05 to 9.60

Static Longitudinal Stability Characteristics of Various Mercury Escape Configurations and of a Proposed Alternate Escape Configuration for Mach Numbers of 0.05 to 9.60 PDF Author: Robert P. Smith
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 180

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Book Description