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Sunday, July 26, 2020 | History

3 edition of optimization study of the UTIAS implosion-driven hypervelocity launcher MK II found in the catalog.

optimization study of the UTIAS implosion-driven hypervelocity launcher MK II

Robert Finch Flagg

optimization study of the UTIAS implosion-driven hypervelocity launcher MK II

by Robert Finch Flagg

  • 59 Want to read
  • 12 Currently reading

Published by Institute for Aerospace Studies, University of Toronto] in [Toronto .
Written in English

    Subjects:
  • Hypervelocity guns.,
  • Shock tubes.

  • Edition Notes

    Includes bibliographical references.

    Statementby Robert F. Flagg and Gregory P. Mitchell.
    SeriesUTIAS technical note ;, no. 130
    ContributionsMitchell, Gregory P., joint author.
    Classifications
    LC ClassificationsTL507 .T6 no. 130, TL567.S4 .T6 no. 130
    The Physical Object
    Paginationv, 20 p.
    Number of Pages20
    ID Numbers
    Open LibraryOL4074691M
    LC Control Number79886060


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Optimization study of the UTIAS implosion-driven hypervelocity launcher MK II by Robert Finch Flagg Download PDF EPUB FB2

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Schematic of a linear implosion driven hypervelocity launcher, showing stages of explosive operation. Jason Loiseau et al. / Procedia Engineering 58 () 77 – 87 79 by: 8. Procedia Engineering 58 () 77 – 87 The Authors. Published by Elsevier Ltd. Selection and peer-review under responsibility of the Hypervelocity Impact Society doi: / The 12 th Hypervelocity Impact Symposium Development of a Linear Implosion-Driven Hypervelocity Launcher Jason Loiseau a *, Justin Huneault a, Andrew J.

Higgins a Cited by: 8. Development of a Linear Implosion-driven Hypervelocity Available via license: CC BY-NC-ND The launcher presented in this study uses explosives to operate the pump.

Work carried out on the development of a single‐stage implosion‐driven hypervelocity launcher is presented. Explosives surrounding a thin‐walled tube filled with helium works similar to the pump tube of a conventional light gas gun. Implosion of the tube drives a strong shock that reflects back and forth between the projectile and the implosion pinch, generating very high temperatures Cited by: 2.

Abstract. A hypervelocity impact is an impact event where the relative velocity (V) between two colliding objects is close to or exceeds the speed of sound (C 0) in each of the object’s materials (usually V > 4 [km/s]).During such an impact, a large amount of kinetic energy is released within a very short time, and supersonic compression shock waves are formed at the contact surface Author: A.

Devir, A. Lessin, A. Vaynshtein. UTIAS implosion-driven hyperveloclty launcher, Mark II, cavity 8 in dla., barrel 0 22 in_ dia x 2 ft long UTIAS IMPLOSION-DRIVEN HYPERVELOCITY LAUNCHERS AND SHOCK TUBES Figure 10 shows a perspective view of the in.-dia. launcher (Mark II--the drawings were subsequently modified for the Mark III launcher).Cited by: Full text of "President's report for the year ended June (part one and two)" See other formats.

Superconducting millimetre-wave cameras. NASA Astrophysics Data System (ADS) Monfardini, Alessandro. I present a review of the developments in kinetic inductance detec.

Microscale shock tube. NASA Astrophysics Data System (ADS) Mirshekari, Gholamreza. This project aims at the simulation, design, fabrication and testing of a microscale shock tube.