I would like to see the su 47 in the game as a fun plane because of its uniqe design especially on the wings that could bring interesting flight performance. search su 47 to see a picture of it.
to make it easier so see some performance statistiks here are some:
speed: sea level: mach 1.12 1,400 km/h (870 mph; 760 kn) and at altitude mach 2.21 2,200 km/h (1,400 mph, 1,200 kn).
climb rate: 233m/s
cruise speed: 1,800km/h
max altituse/service sealing: 18,000m
range: 1,782nm (3,300km)
max takeoff weight is: 34,000kg
manuverebilety: high subsonic because of wing design.
thrust vectoring: it has thrust vectoring ±20° at 30°/second (with PFU engine modification)
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 × 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 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: 1.00 max take-off weight
1.29 normal take-off weight
Armament
- provision for conformal weapon storage
Avionics
- provision for mission radar in nose and ECM in tail radomes
much of this info comes from the webb and websides i dont know but the last part is from wikepedia.
could not find turn time and take off distance.
payload: cant find info about the capebileties. gaijin if you add this plane because of my idea (if you saw mine and thought it was a good idea) i would apreciate it if i could receve it in game and test it from there.
