[b:3f2ef3c95b]MiG-31E Wings fighter (Fighter Interceptor)[/b:3f2ef3c95b]
[table:3f2ef3c95b]
[row:3f2ef3c95b] [b:3f2ef3c95b] Parameter [/b:3f2ef3c95b]
[col:3f2ef3c95b] the Value of the
[row:3f2ef3c95b] [b:3f2ef3c95b] Crew [/b:3f2ef3c95b]
[col:3f2ef3c95b] 2
[row:3f2ef3c95b] [b:3f2ef3c95b] take-off weight - maximum (kg) [/b:3f2ef3c95b]
[col:3f2ef3c95b] 46 200
[row:3f2ef3c95b] [b:3f2ef3c95b] the Weight of internal fuel - maximum (l) [/b:3f2ef3c95b]
[col:3f2ef3c95b] 18 500
[row:3f2ef3c95b] [b:3f2ef3c95b] the Mass of the fuel in the podvěsech (l) [/b:3f2ef3c95b]
[col:3f2ef3c95b] 2x 2 500
[row:3f2ef3c95b] [b:3f2ef3c95b] Engine [/b:3f2ef3c95b]
[col:3f2ef3c95b] 2x D30F6
[row:3f2ef3c95b] [b:3f2ef3c95b] Thrust with afterburner (kg) [/b:3f2ef3c95b]
[col:3f2ef3c95b] 2x 15 500
[row:3f2ef3c95b] [b:3f2ef3c95b] the Maximum operating overload [/b:3f2ef3c95b]
[col:3f2ef3c95b] 5g
[row:3f2ef3c95b] [b:3f2ef3c95b] Maximum speed (airspeed) in elevation (km/h) [/b:3f2ef3c95b]
[col:3f2ef3c95b] 3 000
[row:3f2ef3c95b] [b:3f2ef3c95b] Maximum speed (airspeed) at sea level (km/h) [/b:3f2ef3c95b]
[col:3f2ef3c95b] 1 500
[row:3f2ef3c95b] [b:3f2ef3c95b] service Ceiling (m) [/b:3f2ef3c95b]
[col:3f2ef3c95b] 20 600
[row:3f2ef3c95b] [b:3f2ef3c95b] the Maximum distance-to-target at a speed of M= 2.35, altitude 18 000 m (km) [/b:3f2ef3c95b]
[col:3f2ef3c95b] 720
[row:3f2ef3c95b] [b:3f2ef3c95b] the Maximum distance-to-target at a speed of M= 0.8, a height of 10 000 m (km) [/b:3f2ef3c95b]
[col:3f2ef3c95b] 1 450
[row:3f2ef3c95b] [b:3f2ef3c95b] the Maximum distance-to-target at a speed of M= 0.8, a height of 10 000 m and one refueling (km) [/b:3f2ef3c95b]
[col:3f2ef3c95b] 2 250
[row:3f2ef3c95b] [b:3f2ef3c95b] take-off Distance available (m) [/b:3f2ef3c95b]
[col:3f2ef3c95b] 1 200
[row:3f2ef3c95b] [b:3f2ef3c95b] the Length of the landing (m) [/b:3f2ef3c95b]
[col:3f2ef3c95b] 800
[row:3f2ef3c95b] [b:3f2ef3c95b] the Required length of the runway (m) [/b:3f2ef3c95b]
[col:3f2ef3c95b] 2 500
[/table:3f2ef3c95b]
Source:
http://www.migavia.ru/.
[table:3f2ef3c95b]
[row:3f2ef3c95b] [b:3f2ef3c95b] Parameter [/b:3f2ef3c95b]
[col:3f2ef3c95b] the Value of the
[row:3f2ef3c95b] [b:3f2ef3c95b] Crew [/b:3f2ef3c95b]
[col:3f2ef3c95b] 2
[row:3f2ef3c95b] [b:3f2ef3c95b] take-off weight - maximum (kg) [/b:3f2ef3c95b]
[col:3f2ef3c95b] 46 200
[row:3f2ef3c95b] [b:3f2ef3c95b] the Weight of internal fuel - maximum (l) [/b:3f2ef3c95b]
[col:3f2ef3c95b] 18 500
[row:3f2ef3c95b] [b:3f2ef3c95b] the Mass of the fuel in the podvěsech (l) [/b:3f2ef3c95b]
[col:3f2ef3c95b] 2x 2 500
[row:3f2ef3c95b] [b:3f2ef3c95b] Engine [/b:3f2ef3c95b]
[col:3f2ef3c95b] 2x D30F6
[row:3f2ef3c95b] [b:3f2ef3c95b] Thrust with afterburner (kg) [/b:3f2ef3c95b]
[col:3f2ef3c95b] 2x 15 500
[row:3f2ef3c95b] [b:3f2ef3c95b] the Maximum operating overload [/b:3f2ef3c95b]
[col:3f2ef3c95b] 5g
[row:3f2ef3c95b] [b:3f2ef3c95b] Maximum speed (airspeed) in elevation (km/h) [/b:3f2ef3c95b]
[col:3f2ef3c95b] 3 000
[row:3f2ef3c95b] [b:3f2ef3c95b] Maximum speed (airspeed) at sea level (km/h) [/b:3f2ef3c95b]
[col:3f2ef3c95b] 1 500
[row:3f2ef3c95b] [b:3f2ef3c95b] service Ceiling (m) [/b:3f2ef3c95b]
[col:3f2ef3c95b] 20 600
[row:3f2ef3c95b] [b:3f2ef3c95b] the Maximum distance-to-target at a speed of M= 2.35, altitude 18 000 m (km) [/b:3f2ef3c95b]
[col:3f2ef3c95b] 720
[row:3f2ef3c95b] [b:3f2ef3c95b] the Maximum distance-to-target at a speed of M= 0.8, a height of 10 000 m (km) [/b:3f2ef3c95b]
[col:3f2ef3c95b] 1 450
[row:3f2ef3c95b] [b:3f2ef3c95b] the Maximum distance-to-target at a speed of M= 0.8, a height of 10 000 m and one refueling (km) [/b:3f2ef3c95b]
[col:3f2ef3c95b] 2 250
[row:3f2ef3c95b] [b:3f2ef3c95b] take-off Distance available (m) [/b:3f2ef3c95b]
[col:3f2ef3c95b] 1 200
[row:3f2ef3c95b] [b:3f2ef3c95b] the Length of the landing (m) [/b:3f2ef3c95b]
[col:3f2ef3c95b] 800
[row:3f2ef3c95b] [b:3f2ef3c95b] the Required length of the runway (m) [/b:3f2ef3c95b]
[col:3f2ef3c95b] 2 500
[/table:3f2ef3c95b]
Source:
http://www.migavia.ru/.