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
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.
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
Author: Amado A. Trujillo
Publisher:
ISBN:
Category : Drag (Aerodynamics)
Languages : en
Pages : 44
Book Description
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
Author: J. T. Best (Jr.)
Publisher:
ISBN:
Category : Drag (Aerodynamics)
Languages : en
Pages : 122
Book Description
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
Author: Robert J. Keynton
Publisher:
ISBN:
Category : Launch vehicles (Astronautics)
Languages : en
Pages : 140
Book Description
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
Some Effects of Aircraft Configuration on Static Longitudinal and Directional Stability Characteristics at Supersonic Mach Numbers Below 3
Author: M. Leroy Spearman
Publisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 22
Book Description
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°
Author: Gerald V. Foster
Publisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 38
Book Description
Publisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 38
Book Description