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RANGE REPORT {design} ____________ {TOW 73500.kg./ OEW 41310.kg./ Fuel 18540.kg./ Payload 13650.kg.} Range mode: 99% max.SAR, step-up cruise Climb schedule: 250./ 278.kcas/ mach 0.732 above 29683.feet Cruise at Mach = 0.781 {FL 350 390} ICA 35000.feet, 450.ktas, 265.kcas, CL=0.62, 4550.lbf./eng=MCR-18% FCA 39000.feet, 448.ktas, 241.kcas, CL=0.61, 3782.lbf./eng=MCR-19% Distance Time Fuelburn (n.miles) (min.) (kg.) _________ ______ _______ Climb 140. 23. 1696. {S.L to ICA} Cruise 2628. 352. 13087. {ICA to ICA} Descent 102. 18. 156. {ICA to S.L} _________ ______ _______ Trip total 2870. 393. 14939. Block total ========= 409. 15389. Emissions: taxi,t/o climb cruise descent app,taxi total (kg.NOx) 2.6 20.2 78.7 0.5 1.3 103.3 (kg.HC) 0.12 0.07 1.56 0.25 0.13 2.13 (kg.CO) 2.0 3.6 51.4 3.7 2.1 62.8 Manoeuvre allowances: taxi-out 92. kg. {extra to t/o mass} 7.5 min. takeoff 125. kg. 1.0 min. approach 172. kg. 3.0 min. taxi-in 61. kg. {taken from reserves} 5.0 min. Reserves {at landing mass 58264.kg.}: Diversion distance 200. n.miles Diversion mach 0.566 Diversion altitude 21413. feet Diversion fuel 1391. kg. Holding time 30. minutes Holding mach 0.300 Holding altitude 5000. feet Holding fuel 1151. kg. Contingency fuel 762. kg. {5.% of mission fuel} Total Reserve fuel 3304. kg. |