The design of the very high manoeuvrability prototype is based on the avionics and aerodynamics technologies developed for the Su-27 upgrade programme.
Some of the systems and component designs from the Su-27, (the all weather supersonic fighter aircraft with Nato reporting name Flanker), have been used in the Su-47, for example the design of the canopy, landing gear, some of the avionics and the near-vertical tails.
Manoeuvrability
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, and it also retains manoeuvrability in supersonic flight.
Maximum turn rates and the upper and lower limits on air speed for weapon launch are important criteria in terms of combat superiority.
The Su-47 aircraft has very high levels of manoeuvrability with maintained stability and controllability at all angles of attack.
Maximum turn rates are important in close combat and also at medium and long range, when the mission may involve engaging consecutive targets in different sectors of the airspace. A high turn rate of the Su-47 allows the pilot to turn the fighter aircraft quickly towards the next target to initiate the weapon launch.
"The Su-47 has extremely high agility at subsonic speeds."
The swept-forward wing, compared to a swept-back wing of the same area, provides a number of advantages: higher lift to drag ratio; higher capacity in dogfight manoeuvres; higher range at subsonic speed; improved stall resistance and anti-spin characteristics; improved stability at high angles of attack; a lower minimum flight speed; and a shorter take-off and landing distance.
Fuselage
The Su-47 fuselage is oval in cross section and the airframe is constructed mainly of aluminium and titanium alloys and 13% by weight of composite materials.
The nose radome is slightly flattened at the fore section and has a horizontal edge to optimise the aircraft's anti-spin characteristics.
Wings
The forward swept midwing gives the unusual and characteristic appearance of the Su-47. A substantial part of the lift generated by the forward-swept wing occurs at the inner portion of the wingspan. The lift is not restricted by wingtip stall. 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.
The wing panels of the Su-47 are constructed of nearly 90% composites. The forward-swept midwing has a high aspect ratio, which contributes to long-range performance. The leading-edge root extensions blend smoothly to the wing panels, which are fitted with deflectable slats on the leading edge; flaps and ailerons on the trailing edge.
The all-moving and small-area trapezoidal canards are connected to the leading-edge root extensions.
Armament
The Su-47 experimental fighter aircraft features 14 hardpoints (2 wingtip, 6–8 underwing, 6-4 conformal underfuselage). The hardpoints are equipped with R-77, R-77PD, R-73, K-74 air to air missiles.
It is also fitted with air to surface missiles X-29T, X-29L, X-59M, X-31P, X-31A, KAB-500, KAB-1500.
Cockpit
The cockpit's design has focused on maintaining a high degree of comfort for the pilot and also on the pilot being able to control the aircraft in extremely high g-load manoeuvres.
"The wing panels of the Su-47 are constructed of nearly 90% composites."
The aircraft is equipped with a new ejection seat and life support system. The variable geometry adaptive ejection seat is inclined at an angle of 60°, which reduces the impact of high G forces on the pilot. The seat allows dogfight manoeuvres with significantly higher g loadings than can normally be tolerated by the pilot.
The pilot uses a side-mounted, low-travel control stick and a tensometric throttle control.
Landing gear
The aircraft uses a retractable tricycle-type landing gear with a single wheel at each unit. The smaller nose wheel retracts towards the rear and the two mainwheels retract forward into the wing roots.
Engine
The Su-47 fighter aircraft is powered by two Perm Aviadvigatel D-30F6 turboshaft engines. Around 83.4kN of dry thurst can be produced by each engine. The engine is principally used in short-haul airplanes for passenger transport.
The length and fantip diameter of the engine are 3,984mm and 1,050mm respectively, while the dry weight and delivery weight of the engine are 1,550kg and 1,712kg respectively. The engine also features a thrust reverser and a low pressure compressor.
Performance
The Su47 fighter aircraft can climb at a rate of 233m/s. It can fly at a maximum speed of 2,500km/h. The range and service ceiling of the aircraft are 1,782nm and 18,000m respectively.
The maximum take-off weight of the aircraft is 34,000kg. The wing loading and maximum g-force of the Su-47 are 360kg/m² and 9g respectively
Dimensions:
Length
22.60m
Wingspan
16.70m
Height
6.36m
Wing Area
61.87m²
Weights:
Empty Weight
24,000kg
Maximum Take-off Weight
34,000kg
Engines:
Type
Perm Aviadvigatel D-30F6
Number
Two
Capacity
83.4kN each
Performance:
Maximum Speed
2,500km/h
Service Ceiling
18,000m
Range
1,782nm
Rate of Climb
233m/s
Wing Loading
360kg/m²
Maximum g-force
Higher than 9g quoted for Su-27
Air Vehicle:
Construction
Airframe
aluminium and titanium alloys
Composites
13% by weight
Data:
Crew
One pilot
Role
Experimental fighter aircraft
Country
Russia
First Delivery
January 2000
Armament:
Air-to-Air Missiles
R-77, R-77PD, R-73, K-74
Air-to-Surface Missiles
X-29T, X-29L, X-59M, X-31P, X-31A, KAB-500, KAB-1500
Key Players:
Manufacturer
Sukhoi Company (JSC)
Operator
Russian Air Force
(From airforce-technology.com)
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