ARO 202 Final Sheet

ARO 202 Final Sheet - Aircraft Weight Payload Weight Calcul...

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Unformatted text preview: Aircraft Weight Payload Weight Calcul GWES 600000 [lbs] Fuel Weight 180000 [lbs] [lbs] [lbs] [lbs] ZFW 420000 [lbs] Payload Weight 100000 [lbs] 300 200 60000 Dry Weight 320000 [lbs] Clean Wing Geometry & Zero Lift Drag Engine Performance (Sea Lev Wingspan 170 [ft] TSFC 0.33 Aspect Ratio 8 [Non-Dim] Max Thrust 60000 Sref 3612.5 [ft^2] # of Engines 3 e 0.9 [Non-Dim] SLS Total Thrust 180000 CDo 0.06 [Non-Dim] Fuel Flow per Engine 19740 Total Fuel Flow 59220 Take-off Wing Geometry Taxi Fuel Weight Take-off Aspect Ratio 7 [Non-Dim] 7% Max T@5 Min. 345.45 Take-off Wing Area 4128.57 [ft^2] Take-off e 0.85 [Non-Dim] Take-off CDo 0.08 [Non-Dim] CDo 0.2 [Non-Dim] 2.2 [Non-Dim] Wing Height 5 Landing Wing Geometry Standard Atmosphere Cal Landing Aspect Ratio 6.8 [Non-Dim] Tsl 518.69 Landing Wing Area 4250 [ft^2] Psl 2116.2 Landing e 0.85 [Non-Dim] Rhosl Landing CDo 0.09 [Non-Dim] LapseRt 2.5 [Non-Dim] g 32.17 Cruise Altitude Temp Temp Press Press Density Density Speed of Sound (feet) (Deg.R) Ratio Ratio (PSF) Ratio (Slug/ft^3) [ft/sec] 518.69 1.0000 1.00000 2116.200 1.000 0.0023770 1116.2888766 1000 515.12 0.9931 0.96435 2040.757 0.971 0.0023081 1112.4406897 2000 511.55 0.9862 0.92974 1967.506 0.943 0.0022408 1108.5791447 3000 507.98 0.9794 0.89613 1896.399 0.915 0.0021750 1104.7041016 4000 504.41 0.9725 0.86352 1827.388 0.888 0.0021107 1100.8154178 5000 500.84 0.9656 0.83188 1760.424 0.862 0.0020479 1096.9129482 6000 497.27 0.9587 0.80118 1695.462 0.836 0.0019864 1092.9965453 7000 493.70 0.9518 0.77141 1632.454 0.810 0.0019265 1089.0660586 8000 490.13 0.9449 0.74254 1571.356 0.786 0.0018679 1085.1213352 9000 486.56 0.9381 0.71455 1512.123 0.762 0.0018106 1081.1622191 10000 482.99 0.9312 0.68742 1454.711 0.738 0.0017548 1077.1885517 # of Passengers Weight per Passenger Passenger Wegiht CLMAX CLMAX 11000 479.42 0.9243 0.66113 1399.077 0.715 0.0017002 1073.2001714 12000 475.85 0.9174 0.63566 1345.178 0.693 0.0016470 1069.1969136 13000 472.28 0.9105 0.61099 1292.974 0.671 0.0015950 1065.1786104 14000 468.71 0.9036 0.58710 1242.422 0.650 0.0015443 1061.1450909 15000 465.14 0.8968 0.56397 1193.482 0.629 0.0014949 1057.0961811 16000 461.57 0.8899 0.54159 1146.116 0.609 0.0014467 1053.0317032 17000 458.00 0.8830 0.51993 1100.283 0.589 0.0013996 1048.9514765 18000 454.43 0.8761 0.49898 1055.946 0.570 0.0013538 1044.8553163 19000 450.86 0.8692 0.47872 1013.067 0.551 0.0013091 1040.7430346 20000 447.29 0.8623 0.45913 971.608 0.532 0.0012656 1036.6144394 21000 443.72 0.8555 0.44019 931.535 0.515 0.0012231 1032.4693351 22000 440.15 0.8486 0.42189 892.810 0.497 0.0011818 1028.3075221 23000 436.58 0.8417 0.40421 855.399 0.480 0.0011415 1024.1287966 24000 433.01 0.8348 0.38714 819.268 0.464 0.0011023 1019.9329507 25000 429.44 0.8279 0.37066 784.383 0.448 0.0010642 1015.7197724 26000 425.87 0.8210 0.35474 750.711 0.432 0.0010270 1011.4890449 27000 422.30 0.8142 0.33939 718.218 0.417 0.0009909 1007.2405472 28000 418.73 0.8073 0.32458 686.874 0.402 0.0009557 1002.9740535 29000...
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ARO 202 Final Sheet - Aircraft Weight Payload Weight Calcul...

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