Su-47 Berkut
The only Su-47 at an airshow in 2008.
Role	Experimental aircraft/Technology demonstrator Type of aircraft
Manufacturer	Sukhoi
Designer	Mikhail Pogosyan
First flight	25 September 1997
Status	Cancelled
Primary user	Russian Air Force
Number built	1
Developed from	Sukhoi Su-37

The Sukhoi Su-47 Berkut (Russian: Сухой Су-47 Беркут, lit. 'Golden Eagle') (NATO reporting name Firkin^[1]), also designated S-32 and S-37 (not to be confused with the twin-engined delta canard design^[2] offered by Sukhoi in the early 1990s under the designation Su-37) during initial development, was a Russian experimental supersonic jet fighter developed by the JSC Sukhoi Company. A distinguishing feature of the aircraft was its forward-swept wing^[3] that gave the aircraft excellent agility and maneuverability. While serial production of the type never materialized and the configuration was not further pursued, the sole aircraft produced served as a technology demonstrator prototype for a number of advanced technologies later used in the 4.5 generation fighter Su-35 and current fifth-generation jet fighter Su-57.

Development

Originally known as the S-37, Sukhoi redesignated its advanced test aircraft as the Su-47 in 2002. Officially nicknamed Berkut (Russian: Беркут) (the Russian word for the golden eagle), the Su-47 was originally built as Russia's principal testbed for composite materials and sophisticated fly-by-wire control systems, as well as new airframe technologies.

TsAGI has long been aware of the advantages of forward-swept wings, with research including the development of the Tsibin LL and study of the captured Junkers Ju 287 in the 1940s. At high angles of attack, the wing tips remain retracted allowing the aircraft to retain aileron control. Conversely to more conventional rear-swept wings, forward sweep geometrically creates increased angle of incidence of the outer wing sections when the wing bends under load. The wings experience higher bending moments, leading to a tendency for the wings to fail structurally at lower speeds than for a straight or aft-swept wing.

The project was launched in 1983 on order from the Soviet Air Force. But when the USSR dissolved, funding was frozen and development continued only through funding by Sukhoi.^{[citation needed]} Like its US counterpart, the Grumman X-29, the Su-47 was primarily a technology demonstrator for future Russian fighters such as the Sukhoi Su-57. The forward-swept wing configuration was ultimately not pursued because it was mainly advantageous at transonic speeds while an aft-swept wing was superior at supersonic speeds.^[4]

Design

Outline of the Sukhoi Su-47

The Su-47 is of similar dimensions to previous large Sukhoi fighters, such as the Su-35. To reduce development costs, the Su-47 borrowed the forward fuselage, vertical tails, and landing gear of the Su-27 family. Nonetheless, the aircraft includes an internal weapons bay, and space set aside for an advanced radar.

Like its immediate predecessor, the Su-37, the Su-47 is of tandem-triple layout, with canards ahead of wings and tailplanes. The Su-47 has two tailbooms of unequal length outboard of the exhaust nozzles. The shorter boom, on the left-hand side, houses ECM system, while the longer boom houses a rear-facing radar.

Maneuverability

The Su-47 has extremely high agility at subsonic speeds, enabling the aircraft to alter its angle of attack and its flight path very quickly while retaining maneuverability in supersonic flight.^{[citation needed]}

Wings

The forward-swept midwing gives the Su-47 its unconventional appearance. A substantial part of the lift generated by the forward-swept wing occurs at the inner portion of the wingspan. This inboard lift is not restricted by wingtip stall^{[citation needed]} and the lift-induced wingtip vortex generation is thus reduced. The ailerons—the wing's control surfaces—remain effective at the highest angles of attack, and controllability of the aircraft is retained even in the event of airflow separating from the remainder of the wings' surface.

A downside of such a forward-swept wing design is that it geometrically produces wing twisting as it bends under load, resulting in greater stress on the wing than for a similar straight or aft-swept wing. This requires the wing be designed to twist as it bends—opposite to the geometric twisting. This is done by the use of composites wing skins laid-up to twist. The plane was initially limited to Mach 1.6. Because the forward sweep was primarily beneficial at transonic speed while losing out to aft-swept wing at supersonic speed, it was not further pursued.

Thrust vectoring

The thrust vectoring (with PFU engine modification) of ±20° at 30°/second in pitch and yaw will greatly support the agility gained by other aspects of the design.

Specifications (Su-47)

Data from Jane's All the World's Aircraft 2000–01^[5]

General characteristics

• Crew: 1
• Length: 22.6 m (74 ft 2 in)
• Wingspan: 16.7 m (54 ft 9 in)
• Height: 6.4 m (21 ft 0 in)
• Wing area: 56 m² (600 sq ft)
• Airfoil: 5%
• Gross weight: 25,670 kg (56,593 lb)
• Max takeoff weight: 34,000 kg (74,957 lb)
• Powerplant: 2 × Soloviev D-30F6^[6] afterburning turbofan engines, 93.1 kN (20,900 lbf) thrust each engines with 2-dimensional and 3-dimensional thrust-vectoring nozzles planned for testing. dry, 153 kN (34,000 lbf) with afterburner

Performance

• Maximum speed: 2,200 km/h (1,400 mph, 1,200 kn) / M2.21 at altitude

1,400 km/h (870 mph; 760 kn) / M1.12 at sea level

• Range: 3,300 km (2,100 mi, 1,800 nmi)
• Service ceiling: 18,000 m (59,000 ft)
• g limits: +9
• Rate of climb: 233^[7] m/s (45,900 ft/min)
• Wing loading: 607 kg/m² (124 lb/sq ft) max (approx.)

458 kg/m² (94 lb/sq ft) normal (approx.)

• Thrust/weight: 0.92 max take-off weight

1.21 normal take-off weight

Armament

• provision for conformal weapon storage

Avionics

• provision for mission radar in nose and ECM in tail radomes

Gallery