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 Download

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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 at Mach Numbers from 3.0 to 6.8 of the Static Aerodynamic Characteristics of Modified Mercury Exit and Escape Capsule Configurations

Wind-tunnel Investigation at Mach Numbers from 3.0 to 6.8 of the Static Aerodynamic Characteristics of Modified Mercury Exit and Escape Capsule Configurations PDF Author: Albin O. Pearson
Publisher:
ISBN:
Category : Hypersonic wind tunnels
Languages : en
Pages : 26

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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 at Mach Numbers from 3.0 to 6.8 of the Static Aerodynamic Characteristics of Modified Mercury Exit and Escape Capsule Configurations

Wind-tunnel Investigation at Mach Numbers from 3.0 to 6.8 of the Static Aerodynamic Characteristics of Modified Mercury Exit and Escape Capsule Configurations PDF Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 24

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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 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 : 30

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Wind-tunnel Investigation at Mach Numbers from 0.20 to 1.17 of the Static Aerodynamic Characteristics of a Possible Reentry Capsule

Wind-tunnel Investigation at Mach Numbers from 0.20 to 1.17 of the Static Aerodynamic Characteristics of a Possible Reentry Capsule PDF Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 30

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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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Wind Tunnel Investigation at Mach Numbers from 0.20 to 1.17 of the Static Aerodynamic Characterictics of a Possible Reentry Capsule

Wind Tunnel Investigation at Mach Numbers from 0.20 to 1.17 of the Static Aerodynamic Characterictics of a Possible Reentry Capsule PDF Author: Albin O. Pearson
Publisher:
ISBN:
Category :
Languages : en
Pages : 26

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Book Description

Investigation of Aerodynamic Effects of External Combustion Below Flat-plate Model in 10- by 10-foot Wind Tunnel at Mach 2.4

Investigation of Aerodynamic Effects of External Combustion Below Flat-plate Model in 10- by 10-foot Wind Tunnel at Mach 2.4 PDF Author: Robert G. Dorsch
Publisher:
ISBN:
Category : Mach number
Languages : en
Pages : 30

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Wind Tunnel Investigation of Three Axisymmetric Cowls of Different Lengths at Mach Numbers from 0.60 to 0.92

Wind Tunnel Investigation of Three Axisymmetric Cowls of Different Lengths at Mach Numbers from 0.60 to 0.92 PDF Author: Richard J. Re
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 292

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Book Description