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MiG-25
Mach 3 rocket launch aircraft. Mikoyan Interceptor-cropped delta. Maximum release conditions: Wing mounted, 750 kg (6.3 m length x 2.2 m wingspan) at 3,161 kph at 24,000 m altitude

Status: Out of Production. Payload: 750 kg (1,650 lb). Thrust: 182.34 kN (40,993 lbf). Gross mass: 32,136 kg (70,847 lb). Unfuelled mass: 19,995 kg (44,081 lb). Specific impulse: 2,073 s. Specific impulse sea level: 1,884 s. Burn time: 3,000 s. Height: 22.31 m (73.19 ft). Diameter: 5.60 m (18.30 ft). Span: 13.99 m (45.89 ft). Location: 880.

Cost $ : 40.000 million. No Engines: 2. Release velocity: 880 m/s (2,880 ft/sec). Release altitude: 24 m (78 ft). Release conditions: 3,161 kph at 24 km.



Country: Russia. Engines: R-31 engine. Propellants: Air/Kerosene.

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