DID YOU KNOW? DTIC has over 3.5 million final reports on DoD funded research, development, test, and evaluation activities available to our registered users. Click
HERE to register or log in.
Accession Number:
AD0725807
Title:
The MK II UTIAS Implosion-Driven Hypervelocity Launcher Design Analysis.
Descriptive Note:
Technical note,
Corporate Author:
TORONTO UNIV (ONTARIO) INST FOR AEROSPACE STUDIES
Report Date:
1971-02-01
Pagination or Media Count:
39.0
Abstract:
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 launcher facility, the design of a 30 in. dia. hypervelocity launcher was completed, and a set of detailed workshop were prepared. The report describes the basic functioning of the implosion-driven hypervelocity launcher, as well as its mechanical design, operation and firing procedures. A separate section is devoted to the strength requirements and initial stressing. By using a simple analogy with a spherical pressure chamber, the authors endeavour to estimate the plasticelastic stress level, from which some prediction of fatigue life for such a launcher was derived. The last two sections of this report give some recommendations for the proof-testing of the launcher, as well as some basic aspects regarding safety. Author
Distribution Statement:
APPROVED FOR PUBLIC RELEASE