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Sympathetic reaction tests and analysesThe critical separation distances for explosive reactions of a solid rocket propellant were measured. Explosive reactions included low order explosion, low order detonation, and high order detonation. The effects of sample size, shape, damage and temperature on sympathetic reaction were determined experimentally. The sympathetic detonation of small cubes of solid rocket propellant was modelled numerically, using the Eulerian reactive hydrodynamic code 2DE with Forest Fire burn rates. The model was applied to cubes of 2.54 - 7.62 cm (1 - 3 in.), with agreement between calculated and experimental results.
Document ID
19810008646
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Ricardson, D. E.
(Hercules, Inc. Magna, UT, United States)
Bowman, A. L.
(Hercules, Inc. Magna, UT, United States)
Date Acquired
August 11, 2013
Publication Date
December 1, 1980
Publication Information
Publication: NASA, Washington The 1980 JANNAF Propulsion Systems Hazards Subcomm. Meeting, Vol. 1
Subject Category
Propellants And Fuels
Accession Number
81N17166
Funding Number(s)
CONTRACT_GRANT: N00030-74-C-0100
CONTRACT_GRANT: N00030-77-M-077002
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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