iterative take-off weight

Sheet1Mission RequirementsMax. Mach2.1Cruise Mach2.1Cruise Alt. (ft)55,000Oper. Rad. (nm)2,000Engine: TSFC Min.0.9Engine: TSFC Max.2.17Engine: Thrust (lbs)108,540Aspect Ratio2Combat: Time (min)0Combat: Altitude (ft)30,000Loiter: Time (min)10Loiter: Altitude (ft)0Fuel Reserve (%)5Trapped Fuel (%)1Structure Factor0.5Payload: Exp. (lb)0Payload: Non-exp. (lb)4000Iteration 1Iteration 2Iteration 3Iteration 4Iteration 5Iteration 6Iteration 7Weight: T-O (estimated)40,00040,000.0042,232.5090,523.1790,523.170.000.000.00Weight: T-O (final)42,232.5044,366.3490,523.1790,523.170.000.000.00Surplus Empty Wt. (lbs)-2,232.50-2,133.850.000.000.000.000.001. Start-up & T-O39,000.0041,176.6888,260.0988,260.090.000.000.002. Climb & Accel. to Cruise36,153.0038,170.7981,817.1081,817.100.000.000.003a. L/D7.597.597.597.597.597.597.593b. V (f/s)1,925.701,925.701,925.701,925.701,925.701,925.701,925.703c. Cruise to destination29,364.5831,003.4966,454.3866,454.380.000.000.004. Accel. to high speed29,364.5831,003.4966,454.3866,454.380.000.000.005. Combat29,364.5831,003.4966,454.3866,454.380.000.000.006. Drop Exp. Payload29,364.5831,003.4966,454.3866,454.380.000.000.007. Cruise back23,850.8225,182.0053,976.3053,976.300.000.000.007. Loiter23,384.1324,689.2652,920.1552,920.150.000.000.008. Land22,799.5324,072.0351,597.1551,597.150.000.000.00Total Fuel Wt. (lbs)18,232.5019,250.1041,261.5841,261.580.000.000.00Available Empty Wt. (lbs)17,767.5018,982.4045,261.5845,261.580.000.000.00Required Empty Wt. (lbs)20,000.0021,116.2545,261.5845,261.580.000.000.00

&APage &P

Sheet14000042232.496681284590523.168078843890523.168078844890523.168078844800

&APage &PIteration No.T-O Weight

Sheet2

&APage &P

Sheet3

&APage &P

Sheet4

&APage &P

Sheet5

&APage &P

Sheet6

&APage &P

Sheet7

&APage &P

Sheet8

&APage &P

Sheet9

&APage &P

Sheet10

&APage &P

Sheet11

&APage &P

Sheet12

&APage &P

Sheet13

&APage &P

Sheet14

&APage &P

Sheet15

&APage &P

Sheet16

&APage &P