An Optimization Study of the UTIAS Implosion-driven Hypervelocity Launcher MK 2

An Optimization Study of the UTIAS Implosion-driven Hypervelocity Launcher MK 2
Author :
Publisher :
Total Pages : 25
Release :
ISBN-10 : OCLC:1109471752
ISBN-13 :
Rating : 4/5 ( Downloads)

Book Synopsis An Optimization Study of the UTIAS Implosion-driven Hypervelocity Launcher MK 2 by : Robert F. Flagg

Download or read book An Optimization Study of the UTIAS Implosion-driven Hypervelocity Launcher MK 2 written by Robert F. Flagg and published by . This book was released on 1968 with total page 25 pages. Available in PDF, EPUB and Kindle. Book excerpt:


An Optimization Study of the UTIAS Implosion-driven Hypervelocity Launcher MK 2 Related Books

An Optimization Study of the UTIAS Implosion-driven Hypervelocity Launcher MK 2
Language: en
Pages: 25
Authors: Robert F. Flagg
Categories:
Type: BOOK - Published: 1968 - Publisher:

DOWNLOAD EBOOK

An Optimization Study of the UTIAS Implosion-driven Hypervelocity Launcher MK II
Language: en
Pages: 20
Authors: Robert Finch Flagg
Categories: Hypervelocity guns
Type: BOOK - Published: 1968 - Publisher:

DOWNLOAD EBOOK

An Optimization of Study of the Utias Implosion-driven Hypervelocity Launcher Mk Ii
Language: en
Pages: 87
Authors: Robert F. Flagg
Categories: Ballistic ranges
Type: BOOK - Published: 1970 - Publisher:

DOWNLOAD EBOOK

A detailed study is presented of the optimization of the projectile velocity of the proposed UTIAS MK II Implosion-Driven, Hypervelocity Launcher. The projectil
The MK 2 UTIAS Implosion-driven Hypervelocity Launcher Design Analysis
Language: en
Pages: 19
Authors: V. C. D. Dawson
Categories:
Type: BOOK - Published: 1970 - Publisher:

DOWNLOAD EBOOK

The MK II UTIAS Implosion-driven Hypervelocity Launcher Design Analysis
Language: en
Pages: 19
Authors: V. C. D. Dawson
Categories: Hypervelocity guns
Type: BOOK - Published: 1970 - Publisher:

DOWNLOAD EBOOK

Based on initial experiments carried out on the 8 in. dia. implosion-driven hypervelocity launcher, as well as on a preliminary design study of a larger launche