Experimental Magnus and Static Stability Characteristics of Ballistic Projectiles with Various Boattail Angles and Lengths at Mach Numbers from 0.5 Through 2.5

Experimental Magnus and Static Stability Characteristics of Ballistic Projectiles with Various Boattail Angles and Lengths at Mach Numbers from 0.5 Through 2.5
Author: Leroy M. Jenke
Publisher:
Total Pages: 134
Release: 1975
Genre: Ballistics
ISBN:

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The Effect of Propulsive Jet Specific Heat Ratio on Base Pressure at a Freestream Mach Number of 2.18
Language: en
Pages: 28
Authors: H. Ginsberg
Categories:
Type: BOOK - Published: 1965 - Publisher:

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The report documents studies to determine experimentally the effect of thrusting-jet specific heat ratios on missile model base pressure. The tests were conduct
Static Stability Characteristics of a Flat-nose Cylinder with an Extensible Flare at Mach Numbers from 0.60 Through 1.60 (u).
Language: en
Pages: 1
Authors: L. E. RITTENHOUSE
Categories:
Type: BOOK - Published: 1962 - Publisher:

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Static stability and axial-force data are presented for a recoverable data capsule consisting of a flat-nose cylinder with an extensible flare at Mach numbers f
Parachute Recovery Systems
Language: en
Pages: 524
Authors: Theo W. Knacke
Categories: Sports & Recreation
Type: BOOK - Published: 1992 - Publisher:

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The purpose of this manual is to provide recovery system engineers in government and industry with tools to evaluate, analyze, select, and design parachute reco