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Appraisal of UTIAS implosion-driven hypervelocity launchers and shock tubes.A critical appraisal is made of the design, research, development, and operation of the novel UTIAS implosion-driven hypervelocity launchers and shock tubes. Explosively driven (PbN6-lead azide, PETN-pentaerythritetetranitrate) implosions in detonating stoichiometric hydrogen-oxygen mixtures have been successfully developed as drivers for hypervelocity launchers and shock tubes in a safe and reusable facility. Intense loadings at very high calculated pressures, densities, and temperatures, at the implosion center, cause severe problems with projectile integrity. Misalignment of the focal point can occur and add to the difficulty in using small caliber projectiles. In addition, the extreme driving conditions cause barrel expansion, erosion, and possible gas leakage from the base to the head of the projectile which cut the predicted muzzle velocities to half or a third of the lossless calculated values. However, in the case of a shock-tube operation these difficulties are minimized or eliminated and the possibilities of approaching Jovian reentry velocities are encouraging.
Document ID
19730031378
Acquisition Source
Legacy CDMS
Document Type
Other - Collected Works
Authors
Glass, I. I.
(Toronto, University Toronto, Canada)
Date Acquired
August 7, 2013
Publication Date
January 1, 1972
Subject Category
Facilities, Research, And Support
Report/Patent Number
AFOSR-72-2428TR
AD-753252
Accession Number
73A16180
Funding Number(s)
CONTRACT_GRANT: NGR-52-026-023
CONTRACT_GRANT: AF 33(615)-5313
CONTRACT_GRANT: AF-AFOSR-72-2274
Distribution Limits
Public
Copyright
Other

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