Sukhoi Su-27 'Flanker'

Role: air superiority fighter
Origin: Russia
Design: Sukhoi Design Bureau
Production: KnAAPO, IAPO (IAIA), NAPO
Variants:see variant overview
Operators:see operators list

NOTE BY EDITOR:
As often the case with Russian weaponry, derivatives and/orcertain export versions of the Su-27 have been given a new designation.This section about the Su-27 will discuss the basic Su-27 and itsdevelopment. The history, variant, operator, specification and armament lists will however include all variants including those with new designations to givea good overview of the Flanker family. Type specific information, photos, videos and links of the Su-30/33/34/35/37 can be found in seperate dedicated sections to which you will find linksin this section as well as on the aircraft directory main page.

Introduction

The Su-27 was designed by Sukhoi OKB as a heavy fighter for the SovietAir Force (Voenno-Vozdushmiy Sily - VVS) and National (Homeland) Air Defense Forces (Protivo-Vozdushnoi Oborony - PVO) to regain air superiority over theF-15Eagle operated by the US Air Force. In fact, the requirements were basedon the performance of theF-15 adding ten percent. The Sukhoi design fulfilledthe requirements and beyond. The Su-27 is often proclaimed the best and mostsuccessful Russian fighter of the Cold War era.
After the end of the Cold War and USSR, the Sukhoi OKB (often in cooperation with the KnAAPO plant) developed various advanced variantsaimed at prospective foreign customers. The aircraft were marketed at international air shows, putting up superb aerobatic displays. The aircraftperformance both on paper as in aerobatic displays has stunned many enthusiasts and experts alike all over the world. Also, the Flanker has proven its air superiority in combat during severalAfrican wars. The Su-27 and its derivatives are today some of the mostpopular fighters to be discussed by both aviation enthusiasts and experts.

Design

The main feature for the success of the Su-27 design is its aerodynamic configuration,known as 'integrated aerodynamic concept' by its designers. This configurationis one with extremely blended wing and fuselage. The low-aspect ratio trapezoidalmidwing is fitted with large leading-edge root extensions (LERX) and blending into the fuselage creating a single lifting body.
The aircraft has a near-zero static stability and thus require a fly-by-wiresystem. The SDU-10 pitch-only fly-by-wire system controlsthe pitch of the aircraft to ensure stability and controllability for the pilot,increase aerodynamic performance, limit overload and angle of attack when neededand decrease the airframe aerodynamic load.
Two AL-31F afterburning turbofans are placed in seperate, widely spacedengine nacelles that are mounted under the lifting body. The air intakesare fitted with variable ramps.
The Su-27 has twin vertical fins fitted on the outer sides of the fuselageand twin central fins underneath. The airbrake is placed in the center of themid-section of the aircraft behind the cockpit. The tricycle landing gear of Su-27 and Su-27UB has a single wheel on each strut. The nose wheel is fittedwith a mudguard to protect against foreign object damage (FOD).

Systems & Avionics

The basic Su-27 is fitted with the SUV-27 fire control system,which incorporates the RLPK-27 radar sighting system, OEPS-27 electro-optical sighting system, SEI-31 integrated indication system,IFF interrogator and built-in test system. The fire control system in integratedwith the PNK-10 flight navigation system, radio command link, IFF system, data transmissionequipment and EW self-defence system.
The RLPK-27 system and is controlled by the Ts-100 digital computer and includes the N001 pulse-Dopplerlookdown-capable radar with a range of 80-100 km in the front hemisphere and30-40 km in the rear hemispehere for a fighter-sized target. It cansimultaneously track up to ten aerial targets in track-while-scan mode and provide interceptionof the top priority target.
The OEPS-27 electro-optical sighting system consist of the OLS-27infrared/laser search-and-track system (IRST) and the Shchel-3UM helmet-mountedtarget designator and is controlled by the Ts-100 digital computer. The OLS-27 sensor is placed forward of the cockpit canopy in the centre. The system acquires and tracks aerial targets by their thermal signatures.The helmet-mounted sight and the laser range finder of the IRST can also beused to visually acquire and determine coordinates of air and surface targets.
The SEI-31 integrated indication system provides flight, navigation and sightingdata on the ILS-31 head-up display (HUD) and CRT. The EW self-defence systemsprovides warning to the crew when illuminated by enemy radar and employsboth passive and active countermeasures. The aircraft is equipped withthe SPO-15 Beryoza RWR and APP-50 IR decoy dispenser. Chaff dispensers areplaced in the tail section between the engine nozels. In addition, theaircraft can carry the Sorbtsiya active ECM pods on its wingtips.

Cockpit

The cockpit is fitted with the K-36DM Series 2 ejection seat. The seat-backis being inclined at an angle of 17 degrees. In thetwo-seat Su-27UB version, the seats are placed in tandem with the rear-seat beingelevated to ensure good forward vision. The basic Su-27 cockpit layout consist ofanalogue instruments, HUD and CRT display to display data from radarand electro-optical sight (IRST). On both sides of the HUD control panel, there are sensors for the helmet-mounted target designator system. On the right side below theCRT display the RWR indicator is placed.

Weapons

The Su-27 is fitted with one GSh-301 automatic single-barrel 30mm cannon fitted inside the starboard wing LERX.It can be armed with up to 150 high explosive incendiary or armour piercing tracer rounds.
The basic Su-27's primary armament consists up to six R-27R/ER semi-active radar homer orR-27T/ET heatseeking homer medium range air-to-air missiles, as well as fourR-73 IR agile all-aspect short range air-to-air missile. The basic Su-27 has only a limited air-to-surface capability consisting of onlyunguided bombs and rockets.
See also Armament page

Upgrading the Russian Air Force Su-27 fleet

The Russian Air Force received its first batch of upgradedSu-27s in 2006. The air force seems to have settled for the mid-life upgrade offeredby KnAAPO based on theSu-30MK2, which brings the aircraft up to Su-27SM standard. The Su-27SM is equipped with an upgradedfire control system including the improvedN001V radar with phased array antenna, which offers improved performance andair-to-surface mode. The new system enables theuse of the RVV-AE (R-77) medium range air-to-air missile and a wide selectionof guided air-to-surface bombs and missiles. Another heavily updated featureis the cockpit, which is upgraded with three MFD, new HUD, satellite receiverand new communications set. The aircraft's self-defense suite has also been upgraded.
The Russian Air Force plans to upgrade its entire fleet to Su-27SMstandard, but the exact number of aircraft involved remains unclear.

The Su-27SM is based on earlier proposed upgrades for the Su-27SK exportversion. The Su-27SMK as it is designated has seen two attempts, with at the basisa different radar system (N001M and N001VEP respectively). China was seen as the premier customer for an upgrade package. However Chinaopted to expand its Flanker fleet with multi-roleSu-30MKK and Su-30MKK2instead of upgrading its Su-27SK and J-11 single-seaters. Instead China plannedan indigenous upgrade for its J-11s. Other clients also preferredtwo-seatSu-30MK/MK2. From 2002 onwards, Sukhoi and KnAAPO developed a new deeply modernized single-seat Su-27 derivative known asSu-27BM. DesignatedSu-35, it will be offered for new export orders, replacing the previously offered Su-35, which was based on theSu-27M and offered in the 1990s.

Based on theSu-35 (Su-27BM), the Su-27SM2upgrade is on offer to the Russian Air Force for the second phase of its Su-27 mid-life upgradeprogram. The Su-27SM2 upgrade will give Russia's existing Su-27s a similar avionics and weaponssuite as offered on theSu-35 (Su-27BM). The RussianAir Force has expressed interest in the Su-35, but it remains to be seen whether this willinclude new air frames or be limited to the Su-27SM2 upgrade.

Upgraded Su-27 Flankers for the Russian Air Force are also planned to be fitted with upgraded engines. BothMMPP Salyut and NPO Saturn have developed modernized and more powerful AL-31F variants.In December 2006, the MMPP Salyut's AL-31F-M1 turbofan passed state acceptance tests for useon the Su-27SM. The AL-31F-M1 produces 132.4 kN (29,765 lb) of thrust in an additional mode, 9.8 kN (2,203 lb) more than the standard AL-31F turbofan. It will be followed by the AL-31F-M2 and the even more powerful AL-31F-M3 with 147.1 kN (33,069 lb) of thrust is also under development to compete for the first stage of the PAK-FA program, Russia's future fifth generation fighter. Rival NPO Saturn meanwhile developed theizdelye 117S, another AL-31F derivative based on the AL-41F which produces 142.2 kN maximum thrust. Co-funded by Sukhoi and UMPO, the 117S will enter series production both at Saturn and UMPO to power theSu-35 export fighters. On Febuary 19, 2008, the firstSu-35 prototype made its maiden flight poweredby two 117S. NPO Saturn is also competing to power the PAK-FA with a further modified 117S. Pendinga decision on the powerplant selection for the 'first stage' of the PAK-FA program, it remains to be seenwhich of the options will power the Su-27SM/SM2 upgrades.

The two-seat aircraft will most likely be upgraded to Su-27UBM. AlthoughIAPO offered such an upgrade demonstrated on theSu-30KN, it remains unclear whether the Russian Air Force has opted for this upgrade orplans to have KnAAPO update the two-seaters under a similar program as theSu-27SM/SM2.

For more information regarding the variousupgrades and developments,see the variant overview.