Air Power Series>1:72 die-cast display model>Su-27>HA6011
Su-27SM "Flanker B" Mod. I Red 76, Russian Air Force, 2016
General Background
The Su-27S (NATO reporting name – Flanker) is a single-seat highly-maneuverable
fighter aircraft built by Sukhoi Design Breau as the Soviet response to the U.S. F-14 and
F-15 and entered service in 1985. The primary role of the Su-27 was to provide defense
against American bombers, USN ships and provide Soviet bomber escorts. There have
been many improvements over the years resulting in numerous variants of the Su-27.
The export variant, the Su-27SK was sold to China and eventually developed into the
license-built Shenyang J-11.
The Aircraft
Between 2004 – 2009 54 Su-27S and P variants were upgraded to Su-27SM (serial
modernization). The upgrade included a better fire control system; new radar with a
phased array antenna that allowed for an air-to-surface mode and a larger assortment
of armament. Three MFD (multi-function displays), a HUD; a new self-defense system
along with satellite communications gave an extended life to the Su-27s but are now
being replaced by the Su-35. As new Su-35s arrived at Dzemgi IAP the 12 Su-27SMs
were transferred with Red 76 RF-95261 going to the Besovets IAP.
Specifications :
Manufacturer: | Sukhoi OKB |
Role: | Multi-role Air Superiority Fighter |
Crew: | 1 Pilot |
Dimensions | |
Length: | 21.935 m (71.96 ft) |
Wingspan: | 14.7 m (48.2 ft) |
Height: | 5.932 m (19.45 ft) |
Weight: | |
Empty: | 16,300 kg (35,935 lbs) |
Normal Takeoff : | 23,000 kg (50,706 lbs) |
Maximum Takeoff: | 28,000 kg (61,730 lbs) |
Performance | |
Power Plant: | 2 X Saturn/Lyul'ka AL-31F afterburning turbofans |
Dry Thrust: | 75.22 kN (16,910 lbf) per engine |
Afterburner Thrust: | 122.6 kN (27,560 lbf) per engine |
Fuel Capacity: | 11,975 l (3,163 U.S. Gallons) |
Maximum speed: | @ Altitude 2,500 km/h (1,553.43 mph) |
@ Sea Level 1,400 km/h (870 mph) | |
Maximum Mach: | 2.35 |
Service Ceiling : | 18,500 m (60,696 ft) |
Range: | High Altitude 3,900 km (2,423 miles) |
Sea Level 1,400 km (870 miles) | |
Maximum G-Load: | .9 |
Takeoff Run: | 650 m (2,132 ft) |
Armament: | |
Gun: | 1 X 30 mm GSh-301 Cannon with 149 Rounds |
Hardpoints: | 8 X External Plus 2 X Wingtip Rails |
Missiles: | Air-To-Air R-60/AA-8 Aphid, R-27/AA-10 Alamo,R-73/AA-11 Archer, R-33/AA-9 |
Amos: | Air-To-Ground NONE |
Bombs: | Dumb, Cluster |
Pods: | Rocket and ECM |