Recovery System Design Guide PDF Download

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Recovery System Design Guide

Recovery System Design Guide PDF Author: E. G. Ewing
Publisher:
ISBN:
Category : Parachutes
Languages : en
Pages : 502

Book Description
This document serves as the third revision of the USAF Parachute Handbook which was first published in 1951. The data and information represent the current state of the art relative to recovery system design and development. The initial chapters describe representative recovery applications, components, subsystems, material, manufacture and testing. The final chapters provide empirical data and analytical methods useful for predicting performance and presenting a definitive design of selected components into a reliable recovery system.

Recovery System Design Guide

Recovery System Design Guide PDF Author: E. G. Ewing
Publisher:
ISBN:
Category : Parachutes
Languages : en
Pages : 502

Book Description
This document serves as the third revision of the USAF Parachute Handbook which was first published in 1951. The data and information represent the current state of the art relative to recovery system design and development. The initial chapters describe representative recovery applications, components, subsystems, material, manufacture and testing. The final chapters provide empirical data and analytical methods useful for predicting performance and presenting a definitive design of selected components into a reliable recovery system.

Summary of Static Stability and Drag Characteristics of Axisymmetric Low-drag Shapes for the Subsonic to Hypersonic Mach Number Range

Summary of Static Stability and Drag Characteristics of Axisymmetric Low-drag Shapes for the Subsonic to Hypersonic Mach Number Range PDF Author: Amado A. Trujillo
Publisher:
ISBN:
Category : Drag (Aerodynamics)
Languages : en
Pages : 44

Book Description


Static Stability and Drag Characteristics of a Hypersonic Aircraft Design at Mach Numbers 1.5 to 5.6

Static Stability and Drag Characteristics of a Hypersonic Aircraft Design at Mach Numbers 1.5 to 5.6 PDF Author: J. T. Best (Jr.)
Publisher:
ISBN:
Category : Drag (Aerodynamics)
Languages : en
Pages : 122

Book Description


Longitudinal Stability Characteristics of Preliminary Configurations for Scout D at Mach Numbers 0.20 to 4.63

Longitudinal Stability Characteristics of Preliminary Configurations for Scout D at Mach Numbers 0.20 to 4.63 PDF Author: Robert J. Keynton
Publisher:
ISBN:
Category : Launch vehicles (Astronautics)
Languages : en
Pages : 140

Book Description


Longitudinal Aerodynamic Characteristics at Mach Numbers from 0.50 to 1.19 of a Supersonic Transport Model with a Modified M Wing

Longitudinal Aerodynamic Characteristics at Mach Numbers from 0.50 to 1.19 of a Supersonic Transport Model with a Modified M Wing PDF Author: Edward J. Ray
Publisher:
ISBN:
Category :
Languages : en
Pages : 84

Book Description


Some Effects of Aircraft Configuration on Static Longitudinal and Directional Stability Characteristics at Supersonic Mach Numbers Below 3

Some Effects of Aircraft Configuration on Static Longitudinal and Directional Stability Characteristics at Supersonic Mach Numbers Below 3 PDF Author: M. Leroy Spearman
Publisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 22

Book Description


Stability and Control Characteristics at Mach Numbers of 2.50, 3.00, and 3.71 of a Variable- Wing-sweep Configuration with Outboard Wing Panels Swept Back 75°

Stability and Control Characteristics at Mach Numbers of 2.50, 3.00, and 3.71 of a Variable- Wing-sweep Configuration with Outboard Wing Panels Swept Back 75° PDF Author: Gerald V. Foster
Publisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 38

Book Description


Lateral Directional Stability Characteristics at Mach 2.3 to 3.5 of a Supersonic Transport Model with Various Outboard Vertical-tail Locations

Lateral Directional Stability Characteristics at Mach 2.3 to 3.5 of a Supersonic Transport Model with Various Outboard Vertical-tail Locations PDF Author: William A. Corlett
Publisher:
ISBN:
Category :
Languages : en
Pages : 36

Book Description


Longitudinal and Lateral Aerodynamic Characteristics at Mach Numbers from 0.60 to 4.63 for Two Variable-sweep Configurations

Longitudinal and Lateral Aerodynamic Characteristics at Mach Numbers from 0.60 to 4.63 for Two Variable-sweep Configurations PDF Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 36

Book Description


Lift, Drag, and Static Longitudinal Stability Characteristics of Four Airplane-like Configurations at Mach Numbers from 3.00 to 6.28

Lift, Drag, and Static Longitudinal Stability Characteristics of Four Airplane-like Configurations at Mach Numbers from 3.00 to 6.28 PDF Author: Stanford E. Neice
Publisher:
ISBN:
Category :
Languages : en
Pages : 18

Book Description