Tu-202

Purge model similar to the American bomber B-2 was shown on Central Television in a documentary film "The Fifth Generation."

The project Tu-202 refers to the beginning of the eighties when there is the need to replace distant anti-aircraft Tu-142. The new machine at a lower take-off weight was to have a range of about 16000 km. Later, on the basis of this project were reviewed and other options.

Such B -2 projects were halted in mid-90's. This so-called Tu-202 (built full-scale model) and the MiG.

Bomber was seen as a promising addition to the Tu-160 Blackjack and Tu-95 replacement. As the power plant is probably used bezforsazhny version of NC-32 or its further development.

The main option - strategic bomber, armed with six new cruise missiles X-101 / 102, with a range up to 5500 km.

The bomber is fitted with self-defense in which besides the standard means of electronic protivodeytsviya include four air-to-air missiles and radar sighting rearview.

Based on this platform could be developed following options:

- Strategic bomber, the replacement of the Tu-95MS

- Aircraft ASW (ASW), the replacement of the Tu-142,

- Aircraft reconnaissance and targeting systems, replacement of the Tu-95RTS,

- Tanker.

Estimated characteristics:

                                               202                             V - 2 (U.S.)

length of 23.0 m 21.3 m

span 73.0 m 52.43 m

wing area 526 sq ft 477.52 sq ft

Weight:   

       Max 180000 kg 181,440 kg

        empty 90000 kg 56,700 kg

        fuel up to 70000 kg 74,845 kg

        loads up to 20000 kg 17,420 kg

range 14000 - 16000 km 

Engines 4 x 12 500 kgs

Cruise missile H-101/102

Wing area 04.02 sq ft

Length 9.0 m

Wingspan of 4.5 m

Area:

View from above 8.25 m

Type collection of 4.58 m

Front view of 0.35 m

Volume of 2.36 cubic meters

Density of 1017 kg / m

Off weight 2400 kg

Weight specials. BSc 1 x 130 kg (length 1.0 m, diameter 0.3 m, 200 kT)

Weight 1130 kg of fuel     

WEIGHT 720 kg                        

Equipment weight 220 kg          

Weight std 200 kg     

Range of 5500 km

Flight time 7.5 hours.

Engine P-127-300

Pull 720 kg

Fuel consumption 133 kg / h

Speed

            Max. 800 km / h

            Crace. 720 - 750 km / h

            Min. 570 km / h

Flight altitude of 40 - 110 m

Wing loading 1,015 kg / m

Thrust 0.3

Weight 2200 kg CP
weight of PU with the KR 6 * 2400 kg + 2200 kg = 16600 kg