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A1-Mikoyan-Gourevitch MIG-21bis iz.75A -NFM-000-r2 Acceleration Performances Aircraft : MIG-21bis iz.75A Engine :Tumanskiy R-25-300 CONFIGURATIONS : •DRAG INDEX = 12 (2xR-60 + 2xR-13M) •50% internal fuel •GW= 16,967 lbs / 7,986 kg I – 1 - 40
Time (s) Time (s) Acceleration Diagram A1-Mikoyan-Gourevitch MIG-21bis iz.75A -NFM-000-r2 DATA BASIS : ESTIMATED CONDITIONS: •Standard Day CONDITIONS: •Standard Day •Special AB up to 10,000ft •Max AB from 15,000ft 0 10,000 20,000 Aircraft : MIG-21bis iz.75A Engine :Tumanskiy R-25-300 CONFIGURATIONS : •DRAG INDEX = 12 (2xR-60 + 2xR-13M) •GW=16,967 lbs / 7,986 kg 180 Acceleration (Max Thrust AB) 165 10,000 ft 150 135 120 105 90 75 60 20,000 ft 45 Sea Level 30 15 0 0.30 30,000 0.40 0.50 30,000 0.60 36,000 0.70 0.80 0.90 1.00 1.10 1.20 1.30 1.40 1.50 1.60 Mach 180 Acceleration (Max Thrust AB) 165 150 135 120 105 30,000 ft 36,000 ft 90 75 30,000 ft 60 45 30 15 0 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 Mach I – 1 - 41
Page 1 and 2: A1-Mikoyan-Gourevitch MIG-21bis iz.
Page 3 and 4: Alt (ft) Alt (ft) A1-Mikoyan-Gourev
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 25 and 26: Sustained Load Factor (Ng) Maximum
Page 39: Climb Angle (deg) Excess Specific P

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