Su-33

EJECT

SUKHOI Su-27/30/33/34/35/37 (NATO - Flanker)

VERSIONS – Su-27K (T10K-1), Su-33

Carrier-borne version for the Russian Navy

Fin height

slightly reduced

Arrestor hook

Avionics: revised SDU-10K FCS with 3 channel

FBW, SAU-10K autopilot,TsVM-80-302 processor,

Ts-060K AHRS, A-380 Resistor-B SHORAN, A-723

Kvitok LORAN, ShO-13 Doppler speed drift

system, NSTs-27 HMCS;

Later – SVP-24-33 upgrade with SVP-24 nav/

attack suite (OR-4TM CRT, KAI-24 HUD, SRNS-24

SATNAV/datalink system

2 x Lyul'ka AL-31F Srs 3

afterburning turbofans

Strengthened nose

gear with telescopic

strut and twin nose

wheels

Zvezda K-36K zero-zero

ejector seat inclined at 30º

Revised LERXs (Leading Edge Root eXtensions)

Additional automatically controlled canards

Strengthened airframe

Strengthened main

gear with tie-downs

Single-point refuelling unit relocated to nose wheel bay

Port side retractable

IFR probe

Fuel dump

nozzle in

tail 'sting'

N001K radar

OLS-27K IRST/LR offset to starboard

backup pitot

L006 (SPO-15)

Beryoza RHAWS

in tail 'sting'

Folding wings

and stabilators

for carrier

stowage

Folding outboard

wing section

Wingfold line

L006 (SPO-15)

Beryoza RHAWS

in leading edges

Strakes on

tail 'sting'

ILS-31 HUD, later KAI-24

1 x additional pylon under

each wing (totalling 12)

1 x GSh-301 30 mm

(1.18 in) single-barrel

cannon with 150 rounds

Double-

slotted

flaps

'Wet' centreline pylon for

'buddy' refuelling pod

increased chord to

leading edge flaps

Wing area increased to 67.84 m2 (729.46 ft2)

Su-33 production

(Flanker D)

Carrier-borne version for the Russian Navy

Fin height

slightly reduced

Arrestor hook

Avionics: revised SDU-10K FCS with 3 channel

FBW, SAU-10K autopilot, TsVM-80-302 processor,

Ts-060K AHRS, A-380 Resistor-B SHORAN, A-723

Kvitok LORAN, ShO-13 Doppler speed drift system,

NSTs-27 HMCS

2 x Lyul'ka AL-31F Srs 3

afterburning turbofans

Strengthened nose

gear with telescopic

strut and twin nose

wheels

Zvezda K-36K zero-zero

ejector seat inclined at 30º

Revised LERXs (Leading Edge Root eXtensions)

Additional automatically controlled canards

Strengthened airframe

Strengthened main

gear units with tie-

down shackles

Single-point refuelling unit relocated to nose wheel bay

Port side retractable

IFR probe

Fuel dump

nozzle in

tail 'sting'

N001K radar

OLS-27K IRST/LR offset to starboard

backup pitot

Strakes on

tail 'sting'

Non-folding

wings and

stabilators

taken from

a Su-27UB

1 x additional pylon under

each wing (totalling 12)

1 x GSh-301 30 mm

(1.18 in) single-barrel

cannon with 150 rounds

Su-27K (T10K-1)

first prototype

Back to T10PU-5, Su-30, K, KN, MK, MKI,

MKA, MKK, MK2V, MKV, M2, MKM, SM, SME

Su-27: 10

Go to T-10KUB-1, T10V-1, T10V-2, Su-34

ILLUSTRATIONS: © ADRIAN DAVID MOORE 2015 • NO ITEMS MAY BE REPRODUCED WITHOUT THE PERMISSION OF THE COPYRIGHT HOLDER

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ILLUSTRATIONS: © ADRIAN DAVID MOORE 2015