Chapter 367 (2/2)

Final design parameters of phoenix-1 aircraft:

Wingspan 29.70m

Captain 45.3M

Machine height: 13.67m

Wing sweep angle (outer section) 45.5 °

Empty weight 28 tons

Normal takeoff weight 80 tons

Maximum takeoff weight 88 tons

Maximum carrying capacity 30 tons

The maximum fuel volume is 30 tons

The maximum length of the warehouse is 20m

The maximum width of the warehouse is 2.6m

The maximum height of the warehouse is 2.3m

Maximum flight speed Mach 1.8

Cruise speed Mach 1.1

Practical ceiling 19500m

Sea level climb 109.7 M / S

Take off run distance 1200 meters

Landing run distance 1500 meters

The maximum range is 5100 km

According to the data, this Phoenix aircraft has been very excellent for many people, including many people in Tiangong technology, whether in terms of the maximum flight speed or the maximum flight altitude.

However, the plane can not meet the requirements of Wang Bin's heart, but since it is the first manned plane designed and manufactured by Tiangong technology, Wang Bin also knows that it can't be too demanding.

Moreover, compared with other transport aircraft, this aircraft also has its own defects. First, naturally, as a transport aircraft, the width and height of the cargo warehouse of the Phoenix is too small to carry medium and heavy equipment. For example, there are only a few medium and heavy tanks, even light tanks.

Secondly, in Wang Bin's view, the flight range of this aircraft is still too short, because according to Wang Bin's idea, the flight range of this aircraft should be at least 6000 kilometers, which is qualified, but the flight range of this aircraft is only about 5000 kilometers.

Finally, in terms of the speed and altitude of the aircraft, according to Wang Bin's expectation, it should at least reach the double two standard, that is, Mach 2 and 20000 meters, but the aircraft did not reach the standard.