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|a (TOE)ost897955
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|a (TOE)897955
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|a TOE
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|a E 1.99:ucrl-conf-225607
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|a E 1.99:ucrl-conf-225607
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|a ucrl-conf-225607
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|a LX-17 Deflagration at High Pressures and Temperatures
|h [electronic resource]
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| 260 |
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|a Washington, D.C. :
|b United States. Department of Energy. ;
|a Oak Ridge, Tenn. :
|b distributed by the Office of Scientific and Technical Information, U.S. Department of Energy,
|c 2006.
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| 300 |
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|a PDF-file: 10 pages; size: 0.6 Mbytes.
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| 336 |
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|a text
|b txt
|2 rdacontent.
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|a computer
|b c
|2 rdamedia.
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|a online resource
|b cr
|2 rdacarrier.
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|a Published through SciTech Connect.
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|a 10/23/2006.
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|a "ucrl-conf-225607"
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|a Presented at: Joint Army-Navy-NASA-Air Force 41st Combustion, 29th Airbreathing Propulsion, 23rd Propulsion Systems Hazards Joint Subcommittee Meeting, San Diego, CA, United States, Dec 04 - Dec 08, 2006.
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|a Koerner, J; Maienschein, J; Black, K; DeHaven, M; Wardell, J.
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|a We measure the laminar deflagration rate of LX-17 (92.5 wt% TATB, 7.5 wt% Kel-F 800) at high pressure and temperature in a strand burner, thereby obtaining reaction rate data for prediction of thermal explosion violence. Simultaneous measurements of flame front time-of-arrival and temporal pressure history allow for the direct calculation of deflagration rate as a function of pressure. Additionally, deflagrating surface areas are calculated in order to provide quantitative insight into the dynamic surface structure during deflagration and its relationship to explosion violence. Deflagration rate data show that LX-17 burns in a smooth fashion at ambient temperature and is represented by the burn rate equation B = 0.2P{sup 0.9}. At 225 C, deflagration is more rapid and erratic. Dynamic deflagrating surface area calculations show that ambient temperature LX-17 deflagrating surface areas remain near unity over the pressure range studied.
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|b W-7405-ENG-48.
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|a Ambient Temperature.
|2 local.
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| 650 |
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|a Explosions.
|2 local.
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|a Combustion.
|2 local.
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|a Flames.
|2 local.
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|a Forecasting.
|2 local.
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|a Kel-F.
|2 local.
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|a Pressure Range.
|2 local.
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| 650 |
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|a Propulsion.
|2 local.
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| 650 |
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|a Propulsion Systems.
|2 local.
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| 650 |
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|a Reaction Kinetics.
|2 local.
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| 650 |
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|a Surface Area.
|2 local.
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| 650 |
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|a Tatb.
|2 local.
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| 650 |
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|a Advanced Propulsion Systems.
|2 edbsc.
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| 650 |
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|a Military Technology, Weaponry, And National Defense.
|2 edbsc.
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| 650 |
|
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|a Inorganic, Organic, Physical And Analytical Chemistry.
|2 edbsc.
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| 710 |
2 |
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|a Lawrence Berkeley National Laboratory.
|4 res.
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| 710 |
1 |
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|a United States.
|b Department of Energy.
|4 spn.
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| 710 |
1 |
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|a United States.
|b Department of Energy.
|b Office of Scientific and Technical Information.
|4 dst.
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| 856 |
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|u http://www.osti.gov/scitech/biblio/897955
|z Online Access (via OSTI)
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| 907 |
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|a .b70373115
|b 03-09-23
|c 04-01-12
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| 998 |
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|a web
|b 05-20-19
|c f
|d m
|e p
|f eng
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|h 0
|i 2
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|a Information bridge
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|s 6f62eee4-f40b-5c63-94bf-ca0970fb4931
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| 952 |
f |
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|p Can circulate
|a University of Colorado Boulder
|b Online
|c Online
|d Online
|e E 1.99:ucrl-conf-225607
|h Superintendent of Documents classification
|i web
|n 1
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