Tu-104 Camel
Year deployed | 1956 |
Wing span | 34.54 m |
Length | (A) 38.85m (B) 40.05 m / 130 feet |
Height | 11.90 m |
Wings area | 174.40sq.m (A) 183.50sq.m (B) |
Weight | |
- empty aircraft | 42280kg (A) 43320kg (B) |
- maximum take-off | 76000kg (A) 78100kg (B) |
Max.payload | 9000 kg (A) 12000 (B) |
Engine | 2 TJE AM-3M-500 (RD-3M-500) |
Thrust | 2 x 9700 kgs [93.2 kN] |
Maximum speed | 950 km/h |
Cruising speed | 750-800 km/h |
Range | 3100 km |
Maximum range | 2650 km - 4200km |
Service ceiling | 10000 m |
Crew | 4-5 |
Useful load | 70 (A) 100-115 (B) |
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