natops_flight_manual.. - Check six
natops_flight_manual.. - Check six
natops_flight_manual.. - Check six
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Sustained Load Factor (Ng)<br />
Maximum Available Load Factor (Ng)<br />
Load Factor – Summary<br />
A1-Mikoyan-Gourevitch MIG-21bis iz.75A -NFM-000-r2<br />
DATA BASIS : ESTIMATED<br />
CONDITIONS:<br />
•Standard Day<br />
•Special AB up to 10,000ft<br />
•Max AB from 15,000ft<br />
Aircraft : MIG-21bis iz.75A<br />
Engine :Tumanskiy R-25-300<br />
CONFIGURATIONS :<br />
•DRAG INDEX = 11 (2xR-60)<br />
•GW=16,318 lbs / 7,392 kg<br />
9.00<br />
7.00<br />
Maximum Available Load Factor<br />
0<br />
10,000<br />
20,000<br />
30,000<br />
40,000<br />
5.00<br />
3.00<br />
Max Turn reached without AoA limit<br />
(Stall speed)<br />
Ng < 8 for mach < 0.8<br />
Ng < 6 for mach > 0.8<br />
1.00<br />
0.00 0.20 0.40 0.60 0.80 1.00 1.20 1.40 1.60 1.80 2.00 2.20<br />
Mach number<br />
10.00<br />
9.00<br />
8.00<br />
7.00<br />
Maximum Sustained Load Factor (Ng)<br />
0<br />
10,000<br />
20,000<br />
30,000<br />
40,000<br />
6.00<br />
5.00<br />
4.00<br />
3.00<br />
2.00<br />
1.00<br />
0.00<br />
0.00 0.20 0.40 0.60 0.80 1.00 1.20 1.40 1.60 1.80 2.00 2.20 2.40<br />
Mach number<br />
I - 1 - 6
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