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Military


Tu-104 Camel

Year deployed 1956
Wing span34.54 m
Length(A) 38.85m
(B) 40.05 m / 130 feet
Height11.90 m
Wings area174.40sq.m (A)
183.50sq.m (B)
Weight
- empty aircraft42280kg (A)
43320kg (B)
- maximum take-off76000kg (A)
78100kg (B)
Max.payload 9000 kg (A)
12000 (B)
Engine 2 TJE AM-3M-500 (RD-3M-500)
Thrust2 x 9700 kgs [93.2 kN]
Maximum speed950 km/h
Cruising speed750-800 km/h
Range3100 km
Maximum range2650 km - 4200km
Service ceiling10000 m
Crew4-5
Useful load70 (A)
100-115 (B)



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