VERSIONS – T-10M, Su-35, Su-37, Su-35S, Su-35UB
Modified as thrust-vectoring testbed and redesignated to Su-37, details as T10M-11
(Su-35) unless otherwise indicated
NIIP N011M pulse-
Doppler radar
2 x NPO Lyul'ka-Saturn AL-31FP
afterburning turbofans
Digital FBW (Fly-By-Wire) FCS (Flight Control
System) with quad redundant pitch and triple
redundant yaw/roll systems
Revised cockpit with side-stick controller,
4 x Sextant Avionique LCD displays
Wide-angle HUD
Avionics: revised ESM suite with new SIGINT/
IRINT/RHAWS systems, FADEC (Full Authority
Digital Engine Control), HF/VHF radios,
secure data link/SATCOM systems
Later AL-31FP thrust-vectored turbofans
replaced with non-vectored AL-31F and
revised FCS (Flight Control System)/avionics
AL-100 thrust-
vectoring nozzles
Su-37 (T10M-11)
(Flanker F)
Development of Su-27, LRIP airframe/radar testbed produced
in 1993 details as Su-27 unless otherwise indicated
Taller, squared-off fins with
increased area
2 x Lyul'ka AL-31F afterburning turbofans
Fuel tank
in fins
Strengthened
nose gear with
twin wheels
OLS-27K IRST/LR offset to starboard
Retractable IFR probe
Increased radome
cross section
Revised, strengthened airframe
Revised LERXs (Leading Edge Root eXtensions)
Additional automatically controlled canards
Zvezda K-36DM zero-zero
ejector seat inclined at 30º
1 x GSh-301 30 mm (1.18 in) single-
barrel cannon with 150 rounds
Strengthened
main gear
1 x additional
hardpoint under
each wing
'Glass' cockpit with LCD displays
N011M Bars radar
Revised fuel system
with larger tanks in
wing torsion box
Expanded weapons capabilities
Nose pitot deleted
Avionics: revised WCS, ShO-13-75 Doppler
speed/drift sensor, A-723 LORAN, new RHAWS
suite, BITE (Built-In Test Equipment)
T10M-11 (Su-35)
(Flanker E)
LRIP Su-27M initially used for high alpha/low speed/spin testing,
later re-engined for thrust-vectoring engine tests (shown)
2 x Lyul'ka AL-41F1 afterburning turbofans with thrust-vectoring nozzles
T10M-10
2 x NPO Lyul'ka-Saturn AL-31F afterburning turbofans
Two-seat multi-role combat trainer combining the best features of Su-30MKK/MKI/Su-37, prototype converted from 8th Su-30MKK
Square-tipped fins
increased fin base chord,
area with
integral fuel
tanks
Su-35 avionics/
armament
N011ME radar
Retractable IFR probe
12 x hardpoints
Canards with revised LERXs
Airframe later used as avionics testbed with radar
replaced by Phazotron-NIIR Zhuk-MSE unit, later
converted back to Su-30MKK with canards deleted
Su-35UB
(T10UBM-1)
Taller, squared-off fins with
increased area
Development of Su-27 airframe, details
as Su-27 unless otherwise indicated
New avionics/flight
control system
2 x Lyul'ka AL-31F afterburning turbofans
Fuel tank
in fins
Twin nosewheels
OLS-27K IRST/LR offset
to starboard
Retractable IFR probe
Increased radome
cross section
Revised, strengthened airframe, fuel system
Canards with revised LERXs
T10M-3 (Su-27M,
Su-35) (Flanker E)
2 x NPO Lyul'ka-Saturn AL-41F1S afterburning
turbofans with thrust vectoring
Generation 4++ multi-role fighter based on T10M (Su-35)
incorporating fifth generation fighter technology
Raked fin cap
Revised LERXs, canards deleted
Reprofiled tail
'sting'
Su-27 nose cross section
Strengthened
airframe
Larger rudders
deflecting
outboard to
act as air
brakes
Fin with broader
root chord
Dorsal airbrake deleted
No fin fuel tank
Revised fuel system with increased internal fuel
RAM (Radar Absorbant Material) coatings
applied to leading edges and canopy
Aerosila TA14-130-35
APU on centreline with
intake (to port) and
exhaust (to starboard)
Strengthened nose gear with twin wheels
Strengthened
main gear
Retractable IFR probe
N035 Irbis Phased
array (PESA) radar
UOMZ OLS-35 IRST/LR
offset to starboard
Avionics: Izdeliye 35P FCS, KSU-35 FBW, BINS-SP-2 INS,
S-108 comms suite, Khibiny-M ECM suite (with L-150-35
Pastel RHAWS, Ultraviolet MAWS (Missile Attack Warning
System)), NSTs-T HMCS, Type 4283MP IFF interrogator,
6 x UV-50 chaff/flare dispensers at rear (with 14 rounds
each) 4 x dorsally mounted between tails, 2 x ventrally
mounted
Zvezda K-36D 3.5 zero-
zero ejector seat
RHAWS antenna
Provision for
SAP-518 (L175)
wing tip ECM pod
L-band antenna in wing leading edge
RHAWS antennas
IKSh-1 wide angle
holographic HUD
All-'glass' cockpit
Ultraviolet MAWS sensors
Static electricity zipper
strips on radome
Su-35S
(Flanker E)
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
