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Military


MiG-AT

Specifications
Power plant 2TRD-LARZAC 04R20
Maximum static thrust, kg 2x1,440
Engine maximum take-off power, hp 2x2,20
Wing area, sq.m 17.67
Takeoff weight, kg 4,610
Fuel capacity, normal/total, kg 850/1,680
Thrust-to-weight ratio 0.625
Takeoff speed, km/h 180
Maximum ground-level speed, km/h 850
Max M 0.85
Service ceiling, m 15,500
Maximum operational g-load +8.0 to -3.0
Steady-state turn g-load (H = 4 km, M = 0.7) 5.5
Max permissible angle of attack, deg >25
Flight range, km (H = 6 km, M = 0.5) 1,200
Ferry range, km 2,400
Landing speed, km/h 175
Specific maintenance workload, manhours/flying hours Cw = 2.22
Flying time per flight accident owing to design/production causes, thou h >150
Average flying time before failure and damage revealed in flight and on ground, h Ta = 16.5
Probability of trouble-free operation in flying mission Pfm = 0.9902
Aircraft service life, flying hours 15,000
Operational life, years 30





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Page last modified: 25-10-2021 17:30:07 ZULU