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MiG-25 Foxbat Interceptor-reconnaissance aircraft. First flight: 1964
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Technical specifications

DESIGNER OKB MiG
COUNTRY Russia
TYPE
Interceptor-reconnaissance
CREW 1
POWER-PLANT Two turbojet engines MNPK Soyuz (Khachatourov), R-15BD-300
Thrust, kgf  
- with afterburning 2x11.196
- without afterburner 2x7.500
Thrust-to-weight ratio 0,610
DIMENSIONS  
Length, m 22,30
Length+Pitot, m 23,82
Height, m 6,10
Wing span, m 14,10
Wing area, m2 61,40
Horiontal stabilier span, m 8,5 (an estimated)
WEIGHT  
Maximum take-off, kg 41.000
Normal take-off, kg 36.400
Empty aircraft, kg 20.000
Internal fuel, kg 15.245
Warload, kg 2.000
ΕΠΙΔΟΣΕΙΣ  
Maximum Mach number 2,82
Maximum speed (at high altitude, M=2.83), km/h 3.000
Maximum speed in low height, km/h 1.200
Ferry range, km 2.400
Rate of climb (19.000 m), min 6,6
Service ceiling, m 23.000 (38.000)
Combat range, km 1.250
Range (+4 missiles), km 1.730
Take-off distance, m 500
Landing distance, m 800
Maximum overload, g 5
EQUIPMENT Radar Smerch-A: Detection range 80 km. Range for target jamming 50 km.
Hight resolution cameras with a lateral rotational system.
ARMAMENT It doesn't have a gun. Number external hardpoints: 4. Transportation of weapons: to 2xR-30R, 2xR-30T, R-40R, R-40T, R-60.