Specifications (MiG-25P 'Foxbat-A')
Data from The Great Book of Fighters, International Directory of Military AircraftCombat Aircraft since 1945
General characteristics
- Crew: One
- Length: 19.75 m (64 ft 10 in)
- Wingspan: 14.01 m (45 ft 11.5 in)
- Height: 6.10 m (20 ft 0.25 in)
- Wing area: 61.40 m² (660.93 ft²)
- Empty weight: 20,000 kg (44,080 lb)
- Loaded weight: 36,720 kg (80,952 lb)
- Powerplant: 2 × Tumansky R-15B-300 afterburning turbojets
- Dry thrust: 73.5 kN (16,524 lbf) each
- Thrust with afterburner: 100.1 kN (22,494 lbf) each
Performance
- Maximum speed:
- High altitude: Mach 3.2 (3,600 km/h, 2,170 mph); Mach 2.83 (3,200 km/h, 1,920 mph) continuous engine limit
- Low altitude: 1,200 km/h (648 knots, 746 mph)
- Range: 1,730 km (935 nmi, 1,075 mi) with internal fuel
- Ferry range: 2,575 km (1,390 nmi)
- Service ceiling: 20,700 m (with four missiles) (67,915 ft; over 80,000 ft (24.4 km) for RB models)
- Rate of climb: 208 m/s (40,950 ft/min)
- Wing loading: 598 kg/m² (122.5 lb/ft²)
- Thrust/weight: 0.41
- Time to altitude: 8.9 min to 20,000 m (65,615 ft)
Armament
- 2x radar-guided R-40R (AA-6 "Acrid") air-to-air missiles, and
- 2x infrared-guided R-40T missiles
Avionics
- RP-25 Smerch radar
- A RV-UM or a RV-4 radar altimeter
Read more about this topic: Mikoyan-Gurevich MiG-25