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2su47-2



Su-47 (S-37) Berkut

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David


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Registered: August 2001
Posts: 46,799
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Function: The Su-47 (initially known as the S-37) Berkut (Golden Eagle) is a testbed for developing technologies for the next generation of aircraft.





Description: The basic dimensions and weight of the Su-47 "Berkut" are similar to those of Su-37, although they are different aircraft, and the tail, nose and canopy are similar to those of the Su-35. The first two prototypes of this aircraft were evidently designated the S-32, and the S-37 designation was previously applied to an unrelated fighter project for a smaller delta wing single aircraft that was cancelled due to lack of funding.



The Su-47 features forward-swept wings, which promises a range of benefits in aerodynamics at subsonic speeds and at high angles of attack. The forward-swept wing, which enables the aircraft to increase its range and its manoeuvrability at high altitude, makes extensive use of composite materials. The aircraft has large canards mounted on the intake side, close to the leading edge of the wing. The vertical stabilizers are canted slightly outward [not inward, as previously believed], and two large auxiliary intake doors are visible on the center fuselage section. It is unclear which engines are used on this aircraft. The two powerplants are at the moment D-30F6 turbojets which are normaly used at the MiG-31M, while the second prototype uses the Ljulka AL-37FU turbojet with thrust vectoring. The Su-47 is an experimental program for developing fifth-generation technologies.



The Su-47 is a better performer at high angles of attack in post-stall manoeuvring much needed in close-in dogfight. Having the edge in manoeuvring, the Su-47 is clearly catching up in stealth with US and European new-generation fighters. However even with its internal weapon bay and RAM coating, the new Sukhoi is a very different concept than F-22. The heavy accent on RAM rather than radar absorbing structures (RAS) is obvious. The major components of radar stealth -- RAM coatings and surface quality -- are subject to the production and maintenance tolerance as it was shown by USAF F-117 and B-2 operational experience. Untightened screws, scratches or unfastened access panels were known to greatly deteriorate the RCS of the aircraft, reducing the engineering efforts put into aircraft design. It remains to be seen how Sukhoi will overcome the looser production standards of the Russian aircraft plans.





General Characteristics, Su-47 (S-37) Berkut



Designer:

Sukhoi Design Bureau





Power Plant:

* 2 Perm Aviadvigatel D-30F6 (34,170 lbst), or

* 2 Saturn/Lyul'ka AL-37FU afterburning 142.2 kN (31,966 lb st) with afterburning thrust-vectoring in pitch -20o to 20o at 30o per second





Length:

22.2 m - 22.6 m (72.83 ft - 74.15 ft)





Height:

6.36 m - 6.40 m (20.87 ft - 21.00 ft)





Wingspan:

15.16 m - 16.7 m (49.74 ft - 54.8 ft)





Max Speed:

2,500km/h (1,350 knots)





Ceiling:

18,000 meters (59,055 feet)







Weight:

* Empty: 24,000 kg (52,910 lb)

* Equipped: 26,000 kg (57,320 lb)





Maximum Takeoff Weight:

34,000 kg (74,960 lb)





Range:

1,782 nm (3,300 km/2,050 miles)





Crew:

One





Hardpoints:

14: 2 wingtip, 6-8 underwing, 6-4 conformal underfuselage













· Date: Sat January 3, 2004 · Views: 1959
· Filesize: 20.1kb · Dimensions: 500 x 240 ·
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Keywords: Su-47 (S-37) Berkut


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