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A1-Mikoyan-Gourevitch MIG-21bis iz.75A -NFM-000-r2 Level Flight Envelope I – 1 - 2
Alt (ft) Alt (ft) A1-Mikoyan-Gourevitch MIG-21bis iz.75A -NFM-000-r2 Level Flight Envelope 65,000 60,000 55,000 DATA BASIS : ESTIMATED CONDITIONS: •Standard Day •Max AB 2 x R-60 GW = 16,318 lbs Level Flight Enveloppe Full AB Aircraft : MIG-21bis iz.75A Engine :Tumanskiy R-25-300 Maximal operational mach number (2.02) 50,000 45,000 40,000 35,000 30,000 2 x R-60 490l CL Tank GW = 16,847 lbs Maximal operational mach number with Ext. tank (1.6) 25,000 20,000 15,000 10,000 5,000 Normal A/B Special A/B 1300 Km/h 700 Kts (IAS) 0 0.00 0.10 0.20 0.30 0.40 0.50 0.60 0.70 0.80 0.90 1.00 1.10 1.20 1.30 1.40 1.50 1.60 1.70 1.80 1.90 2.00 2.10 2.20 2.30 2.40 65,000 DATA BASIS : ESTIMATED CONDITIONS: •Standard Day •MILL Power Mach AA1 AA2 AG1 AA4 VNE Level Flight Enveloppe MIL Power Aircraft : MIG-21bis iz.75A Engine :Tumanskiy R-25-300 60,000 55,000 50,000 2 x R-60 GW = 16,318 lbs 45,000 40,000 35,000 30,000 25,000 20,000 15,000 10,000 5,000 2 x R-60 490l CL Tank GW = 17,731lbs 1300 Km/h 700 Kts (IAS) 0 0.00 0.10 0.20 0.30 0.40 0.50 0.60 0.70 0.80 0.90 1.00 1.10 1.20 1.30 1.40 1.50 1.60 1.70 1.80 1.90 2.00 2.10 2.20 2.30 2.40 Mach AA1 AA2 I – 1 - 3
Page 1: A1-Mikoyan-Gourevitch MIG-21bis iz.
Page 5 and 6: Sustained Turn rate (deg/s) Maximum
Page 7 and 8: Turn Rate (degree per second) A1-Mi
Page 19 and 20: Climb Angle (deg) Excess Specific P
Page 21 and 22: A1-Mikoyan-Gourevitch MIG-21bis iz.
Page 25 and 26: Sustained Load Factor (Ng) Maximum
Page 39 and 40: Climb Angle (deg) Excess Specific P
Page 41: Time (s) Time (s) Acceleration Diag

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