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FLUID CrIVT. .4 Il' A � <br /> Er� T _.,,d <br /> TA <br /> ReTank Panel Laminate Thickness,Composition and Propqrttes rft <br /> Pane!Production from same time frame as Proof Tank Panel Production 09-Jan-96 <br /> Ult Flex ' <br /> : Pane! Thick GlassMOE ' <br /> Flex Str Yield Str <br /> J <ln> Yo!•ts ' "10 : *10A223 i ®10^3 osi : Note: Yield Strength was <br /> ' Al 0.303 17.3 1.15 17.55 15;97 ,detemuned for one sample from <br /> each . The yield J A2 0.305 13.1 1.14 19.72 17.95 °was gcaiculpatdeas percent of <br /> 6 !31 0.300 16.1 1.17 19.17 17.44 the ultimate for each sample. <br /> 82 0.326 16.1 1.12 18.14 16.51 `The average of t wse %of <br /> a' C 1 0.326 14.7 1.05 16.51 i 15.02 :ultimate was used to determine tri(. <br /> s C2 0.295 16.9 ° 1.23 r °�° � The an 96 of- ; <br /> 20.67 18.81 ;ultimate was 919x:. All uAirme : <br /> !0 01 : 0.325 15.7 1.13 19.13 i 17.41 !lengths were mullipl eied to <br /> rr: 02 0.376 • 14.1 1.03 15.98 14.54 :determine Oek Yield strengths <br /> E 1 0.361 13.3 1.02 15.06 13.70 j <br /> 13Avg 0.324 15.3 1.12 17.99 r 16.37 t <br /> StdOev 0.026 ` 1.4 ( 0.07 1.76 1,60 t <br /> Ili 95%LCL e i 0.98 14.47 ' 13.17 I <br /> 16! <br /> Panel Location: Paneit were made with 7 R!X ti!ae�ayv>as i <br /> !'; Al 81 j C1 01 E1 <br /> P <br /> ?� A2 82 I C2 02 E2 I <br /> utornate f <br /> =I I a Tensile Tensile ( Flexural ► Flexural o XtJt <br /> -a' Sample Thick t Str OE Stir" Yield Str a MOE <br /> JW 7ptY R-A i 0.203 ! 14.8 ( 14.7 22.51 l 1.766 2724 I 24.52 1.3$0 <br /> �?ptY MMtR.s 0.236 13.2 ! 13.4 19.92 ! 1.510 28.46 1 25.61 1347 <br /> Jr: g 1.64 27.85 ' 25.07 <br /> J.: S dDev 2122 1.38 <br /> JJ' 95%LCL 1.30 r 0.13 0.61 + 0.55 0.02 1 <br /> ' t 18.63 1.38 26.63 23.97 1.33 <br /> JJ <br /> JJ SPty Mat-A ; 0.183 - ' <br /> 20.7 14.67 ; 1.337 i 20.78 I 16.62 1.020 <br /> J6: sPty Mx.B : 0213 18.1 11.92 1.195 ; 20.35 1628 0.912 <br /> J-° aFlyMat.A 0.342 - 17.8 11.80 i 1.227 i 16.34 I 13.07 1.101 <br /> Jai aPty Mat.a '. 0.334 19.3 11.76 1 341 17.59 ; 14 07 1.173 <br /> I <br /> Avg , 12.54 128 18.77 l 15.01 <br /> 1.05 <br /> +o° SdOev 1.23 0.07 1.86 1.49 0.10 I <br /> �r 95X,LCL 10.07 1.14 15.05 12.04 0.86 <br /> J` /s Of Xh mate t"nsth for martyr Jaml)lel ' <br /> 80%. of rrltrmwe urength for the alt prat sample: <br /> fa•ReTank Panels. from the UL Proof testing, were premeasured. The thickness profile of the thinnest <br /> +J;panel was as follows. <br /> ,.; 144" i <br /> Th <br /> 0.353 0.306 0.321 0.328 0.29 0.33 -=-►. AQ 32 ick l <br /> Jo' <br /> 52' : 0.325 0.271 0293 0.277 0.225 0.327 ` I <br /> 0.281 0.306 0.316 0.285 0.305 0.28 02� <br /> JI� � 0.296 <br /> J=' 0.386 0.344 0.287 0.343 0.324 0.346 l 0.338 <br /> JJ: ® ' <br /> t <br /> 5J'Avg Thick 0.336 0.307 0.304 0.354 0.286 0.321 <br /> �I <br />