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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