natops_flight_manual.. - Check six
natops_flight_manual.. - Check six
natops_flight_manual.. - Check six
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Climb Angle (deg)<br />
Excess Specific Power (ft/s)<br />
A1-Mikoyan-Gourevitch MIG-21bis iz.75A -NFM-000-r2<br />
DATA BASIS : ESTIMATED<br />
Aircraft : MIG-21bis iz.75A<br />
Engine :Tumanskiy R-25-300<br />
CONDITIONS:<br />
•Standard Day<br />
•MIL Power<br />
Instantaneous Constant Speed Climb Rate<br />
CONFIGURATIONS :<br />
•DRAG INDEX = 11 (2xR-60)<br />
•GW=16,318 lbs / 7,392 kg<br />
200<br />
100<br />
0<br />
5,000<br />
10,000<br />
15,000<br />
20,000<br />
25,000<br />
30,000<br />
35,000<br />
40,000<br />
45,000<br />
0<br />
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<br />
Mach<br />
Constant Speed Climb Angle<br />
90.00<br />
80.00<br />
70.00<br />
60.00<br />
50.00<br />
40.00<br />
30.00<br />
0<br />
5,000<br />
10,000<br />
15,000<br />
20,000<br />
25,000<br />
30,000<br />
35,000<br />
40,000<br />
20.00<br />
10.00<br />
0.00<br />
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<br />
Mach<br />
I - 1 - 20
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