Wind Tunnel Investigation At Mach Numbers From 050 To 114 Of The Static Aerodynamic Characteristics Of A Model Of A Project Mercury Capsule

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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

Author	: Albin O. Pearson
Publisher	:
Total Pages	: 32
Release	: 1960
Genre	: Space vehicles
ISBN	:

Download 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 Book in PDF, Epub and Kindle

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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

Language: en
Pages: 32

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

Authors: Albin O. Pearson

Categories: Space vehicles

Type: BOOK - Published: 1960 - Publisher:

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

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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

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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

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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

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Categories: Hypersonic wind tunnels

Type: BOOK - Published: 1960 - Publisher:

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

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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

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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

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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

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Type: BOOK - Published: 1960 - Publisher: