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U-2 | ||
Long-range high-altitude reconnaissance plane | ||
Specification: | ||
Year deployed
Wing span, m Length, m Height, m Wings area, m2 Weight, kg - empty aircraft - maximum take-off Internal fuel, l Engine Thrust, kN - dry - afterburner Maximum speed, km/h Cruising speed, km/h Range, km Endurance, h Service ceiling, m Crew |
- 1956 - 24.5 - 15.24 - 4.57 - 55.7 - 6464 - 10954 - 5791.7 - 1 TJE Pratt & Whitney J75-P-13B - 70.28 - 75.62 - 850 - 741 - 4633 - 6 - 21335 - 1 |