JC Wings – Sukhoi Su-27UB Flanker-C , ’68‘ 831st Brigade of Tactical Aviation (Галацький авiаполк, Galatskiy Aviapolk) Ukrainian Air Force

Popis

- sběratelský model letadla  Sukhoi Su-27 Flanker B            1/72
- provedení: kovový model s plastovými částmi
- model je v kvalitním provedení

                          Sukhoi Su-27

Suchoj Su-27 (V kódu NATO „Flanker“) je sovětský dvoumotorový stíhací letoun, určený k boji proti vzdušným cílům ve velkých, středních, malých, přízemních výškách a to ve dne i v noci za každého počasí. Vznikl v konstrukční kanceláři Suchoj. Díky svému značnému doletu může sloužit také jako hlídkový a doprovodný letoun.

The Sukhoi Su-27 (Russian: Сухой Су-27; NATO reporting name: Flanker) is a twin-engine supermaneuverable fighter aircraft designed by Sukhoi. It was intended as a direct competitor for the large United States fourth-generation fighters such as the Grumman F-14 Tomcat and F-15 Eagle, with 3,530-kilometre (1,910 nmi) range, heavy aircraft ordnance, sophisticated avionics and high maneuverability. The Su-27 was designed for air superiority missions, and subsequent variants are able to perform almost all aerial warfare operations. It was designed with the Mikoyan MiG-29 as its complement.

Role	Multirole fighter, air superiority fighter
National origin	Soviet Union / Russia
Manufacturer	Sukhoi
First flight	20 May 1977
Introduction	22 June 1985
Status	In service
Primary users	Russian Air Force People’s Liberation Army Air Force Ukrainian Air Force See Operators section for others
Produced	1982–present
Number built	809
Unit cost	US$30 million
Variants	Sukhoi Su-30 Sukhoi Su-33 Sukhoi Su-34 Sukhoi Su-35 Sukhoi Su-37 Shenyang J-11

Su-27SK

Export Su-27S single-seater. Exported to China in 1992-1996 and developed into Shenyang J-11.

General characteristics

• Crew: 1
• Length: 21.9 m (72 ft)
• Wingspan: 14.7 m (48 ft 3 in)
• Height: 5.92 m (19 ft 6 in)
• Wing area: 62 m² (667 ft²)
• Empty weight: 16,380 kg (36,100 lb)
• Loaded weight: 23,430 kg (51,650 lb) with 56% internal fuel
• Max. takeoff weight: 30,450 kg (67,100 lb)
• Fuel capacity: 9,400 kg (20,724 lb) internal
• Powerplant: 2 × Saturn AL-31F turbofans
  • Dry thrust: 75.22 kN (16,910 lbf) each
  • Thrust with afterburner: 122.6 kN (27,560 lbf) each

Performance

• Maximum speed:
  • At altitude: Mach 2.35 (2,500 km/h, 1,550 mph)
  • At sea level: Mach 1.13 (1,400 km/h, 870 mph)
• Range:
  • At altitude: 3,530 km (2,193 mi; 1,906 nmi)
  • At sea level: 1,340 km (800 mi; 720 nmi)
• Service ceiling: 19,000 m (62,523 ft)
• Rate of climb: 300 m/s (59,000 ft/min)
• Wing loading:
  • With 56% fuel: 377.9 kg/m² (77.3 lb/ft²)
  • With full fuel: 444.61 kg/m² (88.01 lb/ft², 91.98 lb/ft² for Flanker SM.)
• Thrust/weight: 1.07 with 56% internal fuel; 0.91 with full fuel
• Maximum g-load: +9 g

Armament

• Guns: 1 × 30 mm Gryazev-Shipunov GSh-30-1 autocannon with 150 rounds
• Hardpoints: 10 external pylons with a capacity of up to 4,430 kg (9,770 lb)  and provisions to carry combinations of:
  • Rockets:
    • S-8 KOM/BM/OM
    • S-13 T/OF
    • S-25 OFM-PU
  • Missiles:
    • 6 × R-27 R/ER/T/ET/P/EP air-to-air missiles
    • 4 × R-73 E AAMs
  • Bombs:
    • RBK-250 cluster bomb
    • RBK-500 cluster bomb

Avionics

• N001E radar
• Phazotron Zhuk-MSE radar
• Phazotron Zhuk-MSFE radar
• OEPS-27 electro-optical targeting system
• SPO-15 Radar Warning Receiver