Copyright Aviation Week-1965. |
Model Tu-144 SST - CCCP-65000 | ||
Cruising Speed | 2,500 km/h - 1,550 mph (M 2.35) | Copyright Aviation Week-1965. |
Range | 6,500 km - 4,030 ml | |
Gross Weight | 130,000 kg - 286,000 lbs | |
Take-off Run | 1,900 m - 6,240 ft | |
Passengers | 121 |
Although the technical specifications of the plane were indicating 121 seats, the model was presented accidentally with 126
seats, 9 rows of 4 seats for first class (2+2) and 18 rows of 5 seats for tourist class (2+3). We have to think that the
construction process of the prototype had to be very advanced at that time, because the model was very similar to the final
shape and features of the aircraft that performed the first flight in the late day of 1968.
Those features were the four engines mounted side by side in a central group under the fuselage with only two separated air intakes, one for every two engines, the shape of the wing and the huge vertical stabilizer. Is highlighted that one of the most significant systems of the first generation of SST, the droop nose, was not installed in this model. The Soviet delegation at Paris Air Show was the target of the specialized press media present in the fair, trying to discover more info about the plane like number of orders or scheduled date for passenger service. |
Copyright Flight International-1965. |