ShareSukhoi Su-47 Berkut

The Sukhoi Su-47 Berkut (Russian: Су-47 Беркут - Golden Eagle) (NATO reporting name Firkin), also designated S-32 and S-37 (not to be confused with Su-37) during initial development, is an experimental supersonic jet fighter developed by Sukhoi Aviation Corporation. A distinguishing feature of the aircraft is its forward-swept wing, similar to that of the Tsybin's LL-3. The sole aircraft produced is an advanced technology demonstrator prototype and manufacture of a planned second flying prototype is under question due to recent MiG developments of 5th generation Jet fighters. This aircraft is sometimes confused with the single-engined delta canard design offered by Sukhoi in the early 1990s under the S-37 designation.

General characteristics

    * Crew: 1
    * Length: 22.6 m (74 ft 2 in)
    * Wingspan: 15.16 m to 16.7 m (49 ft 9 in to 54 ft 9 in)
    * Height: 6.3 m (20 ft 8 in)
    * Wing area: 61.87 m² (666 ft²)
    * Empty weight: 16,375 kg (36,100 lbs)
    * Loaded weight: 25,000 kg (55,115 lb)
    * Max takeoff weight: 35,000 kg (77,162 lbs)
    * Powerplant: 2× Lyulka AL-37FU(planned) Flying prototypes used 2 Aviadvigatel D-30F6 afterburning, thrust-vectoring (in PFU modification) turbofans with digital control
          o Dry thrust: 83.4 kN (18,700 lbf) each
          o Thrust with afterburner: 142.2 kN (32,000 lbf) each

    * Thrust vectoring: ±20° at 30° per second in pitch and yaw

Performance

    * Maximum speed: Mach 1.6 (Achieved in test flights [3]) (1,717 km/h, 1,066 mph),projected 2710 km/h
      * At sea level: Mach 1.14 (1,400 km/h, 870 mph[1])
    * Cruise speed: projected 1,800 km/h on dry thrust, 2650 km/h on full thrust
    * Range: 3,300 km (2,050 mi)
    * Service ceiling: 18,000 m (59,050 ft)
    * Rate of climb: 233 m/s (46,200 ft/min)
    * Wing loading: 360 kg/m² (79.4 lb/ft²)
    * Thrust/weight: 1.18 when fully loaded,1.15 when empty

Armament

Number of hardpoints: 14: 2 wingtip, 6-8 under wing, 6-4 conformal under fuselage

    * Guns: 1 × 30 mm GSh-30-1 cannon with 150 rounds
    * Missiles: 14 hardpoints (2 wingtip, 6-8 underwing, 4-6 conformal under the fuselage)
          o Air-to-air: R-77, R-77PD, R-73, K-74
          o Air-to-surface: X-29T, X-29L, X-59M, X-31P, X-31A, KAB-500, KAB-1500

Sukhoi Su-37

Sukhoi Su-37 (kode NATO: Flanker-F) adalah pesawat tempur multi-peran buatan Rusia. Su-37 adalah prototipe pesawat buru sergap dan serang berkursi tunggal, segala cuaca, yang dikembangkan dari Su-27. Pesawat ini melakukan tes terbang pertama kali pada bulan April 1996 dari Pusat Ujicoba Terbang 'Zhukovsky' di dekat Moskow.

Operator

Rusia

Spesifikasi (Su-37)

Data dari Gordon and Davison

Karakteristik umum

Kru: 1, pilot

Panjang: 22.183 m (72 ft 9 in)

Lebar sayap: 14.7 m (48 ft 3 in)

Tinggi: 6.43 m (21 ft 1 in)

Area sayap: 62.0 m² (667 ft²)

Berat kosong: 18,500 kg (40,790 lb)

Berat maksimum lepas landas: 35,000 kg (77,160 lb)

Mesin: 2× Lyulka AL-37FU turbofans, 145 kN (32,000 lbf) masing-masing

Performa

Kecepatan maksimum: Mach 2.30 (1,550 mph )

Jarak jangkau: 3,700 km (2,230 mi)

Batas tertinggi servis: 18,000 m (59,100 ft)

Persenjataan

1 × 30 mm GSh-30 cannon with 150 rounds

12 × wing and fuselage stations for up to 8,200 kg (18,080 lb) of ordnance

Pengembangan yang berhubungan

Sukhoi Su-27

Sukhoi Su-30

Sukhoi Su-33

Sukhoi Su-35

Pesawat sebanding

F-15 ACTIVE

F/A-18 HARV

F-16 VISTA

Mikoyan MiG-35

Sumber : Dari Wikipedia bahasa Indonesia, ensiklopedia bebas

Tupolev Tu-160

The Tupolev Tu-160 (Russian: Туполев Ту-160, NATO reporting name: Blackjack) is a supersonic, variable-sweep wing strategic bomber designed by the Soviet Union. Although several civil and military transport aircraft are larger in overall dimensions, the Tu-160 is: the largest combat aircraft, the largest supersonic aircraft and the largest variable-sweep aircraft ever built. The Tu-160 also has the greatest total thrust, and the heaviest takeoff weight of any combat aircraft, and the highest top speed as well as one of the largest payloads of any current heavy bomber.

Entering service in 1987 with the 184 Guards Bomber Regiment, based at Priluki, Soviet Union, the Tu-160 was the last strategic bomber designed by the Soviet Union. The aircraft remains in limited production, with at least 16 currently in service with the Russian Air Force.

Pilots of the Tu-160 call it the “White Swan”, due to its maneuverability and anti-flash white finish.

General characteristics

    * Crew: 4 (pilot, co-pilot, bombardier, defensive systems operator)
    * Length: 54.10 m (177 ft 6 in)
    * Wingspan:
          o Spread (20° sweep): 55.70 m (189 ft 9 in)
          o Swept (65° sweep): 35.60 m (116 ft 9¾ in)
    * Height: 13.10 m (43 ft 0 in)
    * Wing area:
          o Spread: 400 m² (4,306 ft²)
          o Swept: 360 m² (3,875 ft²)
    * Empty weight: 110,000 kg (242,505 lb)
    * Loaded weight: 267,600 kg (589,950 lb)
    * Max takeoff weight: 275,000 kg (606,260 lb)
    * Powerplant: 4× Samara NK-321 turbofans
          o Dry thrust: 137.3 kN (30,865 lbf) each
          o Thrust with afterburner: 245 kN (55,115 lbf) each

Performance

    * Maximum speed: Mach 2.05 (2,220 km/h, 1,200 knots, 1,380 mph) at 12,200 m (40,000 ft)
    * Cruise speed: Mach 0.9 (960 km/h, 518 knots, 596 mph)
    * Range: 12,300 km (7,643 mi) practical range without in-flight refuelling, Mach 0.77 and carrying 6 × Kh-55SM dropped at mid range and 5% fuel reserves[25]
    * Combat radius: 7,300 km[26] (3,994 nmi, 4,536 mi) , 2,000 km (1,080 nmi, 1,240 mi) at Mach 1.5[24]
    * Service ceiling: 15,000 m (49,200 ft)
    * Rate of climb: 70 m/s (13,860 ft/min)
    * Wing loading: 742 kg/m² with wings fully swept (152 lb/ft²)
    * lift-to-drag: 18.5-19, while supersonic it is above 6.[27]
    * Thrust/weight: 0.37

Armament

    * 2 internal bays for 40,000 kg (88,185 lb) of ordnance, options include:

    * 2 internal rotary launchers each holding 6 × Raduga Kh-55 cruise missiles (primary armament) or 12× Raduga Kh-15 short-range nuclear missiles