La-250 Anakonda
There are evidently some problems with the specifications for this aircraft. Published specifications contain some non-trivial variations in key parameters, such as lenght, while normally failing to indicate whether the initial La-250 or the substantially modified La-250A is specified. These uncertainties are reflected in available line art, which is based on inconsistent ratios between the length and wingspan of the aircraft.
| Specifications | ||
|---|---|---|
| Country of Origin | USSR | |
| Builder | Lavochkin | |
| Function | interceptor | |
| Year | La-250 | La-250A |
| Year | 1956 | 1957 |
| Crew | 2 | |
| Length | 25.6m / 83 ft 12 in | 26.80 m / 87 ft 11 in |
| Wingspan | 13.9m / 45 ft 7 in | 13.90 m / 45 ft 7 in |
| height | 6.50 m / 21 ft 4 in | |
| Wing Area | 80.0m2 / 860 sq ft | 80.0 m2 / 860 ft2 |
| Empty Weight | 15,000kg / 33000 lb | 19,000 kg / 42,000 lb |
| Loaded Weight | 24,500 kg / 54,000 lb | |
| Maximum Weight | 26,000kg | |
| Take-off weight | 30000 kg / 66000 lb | 27,500 kg / 60,500 lb |
| number of jets | 2 | 2 |
| Engines | Lyulka AL-7F | Lyulka AL-7F |
| type of jet | turbojets | |
| thrust | 9000kg | 90.2 kN [8950 kgf] [monino] |
| thrust afterburning | 98.0 kN / 22,000 lbf | |
| Maximum Speed Clean | 1,980km/h 2000 km/h / 1250 mph | 1,800 km/h / 1,100 mph 2,000 km/h [monino] |
| Maximum Speed with missiles | 1,600 km/h / 994 mph | |
| Ceiling | 18,500m 18000 m / 59000 ft | 17,000 m / 56,000 ft 18,000 m [monino] |
| Range | 2,800km 2000 km / 1250 miles | 2,000 km / 1,250 mi 2,000 km [monino] |
| loading | 63 lb/ft2 | |
| thrust/weight | 0.41 | |
| Armament |
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