MiG-31 FOXHOUND
| Specifications | |
|---|---|
| Countries of Origin | CIS (formerly USSR) |
| Similar Aircraft | |
| Crew | Two |
| Role | |
| Length | 70 ft, 5 in (21.5 m) |
| Span | 45 ft, 9 in (14 m) |
| Height: | 6.60 m |
| Wing span: | 14.02 m |
| Wing area: | 61.41 sq m |
| Maximum speed: | Mach 2.83 |
| Weight: (empty) | 22,000 kg |
| Weight: (normal) | 36,720 kg |
| Powerplant: | Two Tumanski
R-15BD-300 afterburning turbojets rated at 49.78kN each |
| Maximum Range: | 1,250 km |
| ceiling: |
Zoom to 10,000 meters (33,800 ft) in 8 minutes Service ceiling 20,500 meters (67,250 ft) 20,700 m |
| Rate of climb: | 8 min 54 sec to 20,000 m |
| Ceiling | 24400 meters |
| Cruise range | 1620 nm |
| Take-off mass with fuel: | |
| internal fuel, kg | 41000 |
| with full internal fuel and external fuel, kg | 46200 | Maximum speed: |
| at altitude of 17.5 km max., km/h | 3000 |
| near the ground, km/h | 1500 | Maximum endurance with: |
| external fuel tanks, h | 3.6 |
| with in-flight refueling, h | 6-7 |
| Ferry range, km | 3000 | Intercept range: |
| at the supersonic cruising speed (M 2.35), km | 720 |
| at the subsonic cruising speed (M 0.85) with | 2200 |
| Take-off run, m | 1200 |
| Landing run | 800 |
| In-Flight Refueling | No |
| Internal Fuel | 14200kg |
| Drop Tanks | 2000L drop tank with 1600kg of fuel for 91 nm range |
| Sensors | LD/SD TWS radar, possible IRST, RWR
RP-31E radar sight providing for: |
| Armament |
Typically The MiG-31E is armed with |
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