| Type | Tu-124 | Tu-124V
|
| Function | transport |
|
| Year | 1962 |
|
| Wing Span | 25.55m (83 feet 9.75 inches) | 25.55 m (83 ft 10 in)
|
| Wing Area | 119.37m2 (1280 square. ft) | 119 m² (1,280 ft²)
|
| Length | 31.578m / 30.58 meters (100 feet 4 inches) | 30.58 m (100 ft 4 in)
|
| Height | 8.082mm (26 feet 6 inches) | 8.08 m (26 ft 6 in)
|
| Empty Weight | 22,500kg (49,600 lbs) | 22,500 kg (49,500 lb)
|
| Loaded | | 30,000 kg (67,000 lb)
|
| Maximum Weight | 38,000kg (84,000 pounds) | 38,000 kg (84,000 lb)
|
| Engines | 2*5400kg Soloviev D-20P (11,905 pounds) | 2× Solniev D-20P turbofans; 106 kN (23,800 lbf) thrust
|
| Maximum Speed | 970km/h at an altitude of 8000 meters (26,245 feet) | 907 km/h (490 kt; 564 mph
|
| Fast Cruise | Mach .76 @ 26,250 ft |
|
| Economical Cruise | Mach .73 @ 32,800 ft |
|
| Ceiling | 11,700 meters (38,400 feet) | 11,600 m (38,100 ft)
|
| Rate of climb | | 1,000 m/min (3,300 ft/min)
|
| Wing loading | | 250 kg/m² (52 lb/ft²)
|
| Thrust/weight ratio | | 0.71:1 (7.1 N/kg, 0.71 lbf/lb)
|
| maximum range | 1,300 miles | 2,100 km (1,100 nm; 1,300 sm)
|
| Crew | | 3
|
| Passengers | 44 seats | 56
|
