Каталог - Оружие России 2000 c82-795
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311
PART 2 2
FIGHTERS
GROUP 15 AIRCRAFT AND AIRFRAME
STRUCTURAL COMPONENTS
Class 1510 Aircraft, Fixed Wing
15 ! !
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The MiG-29 is equipped with an in-flight refueling sys-
tem. The aircraft boasts high maintainabilty.
To date, a number of new modifications have been
developed on the basis of the MiG-29 aircraft.
The MiG-29SE is a multirole fighter with an increased
bomb-carrying capacity. The fighter is equipped with
an acquisition/guidance radar jamming station.
The aircraft is furnished with external underwing fuel
tanks. The RVV-AE active radar-homing missiles, car-
ried by the fighter, can be used against two targets
simultaneously.
The MiG-29SM is
able to carry high-
precision air-to-
surface TV-homing
missiles.
The inventory of
guided weapons
intended for defeat-
ing aerial and
ground targets has
been extended
owing to:
- RVV-AE air-to-air
missiles (up to 4
pcs);
- Kh-29T air-to-sur-
face missiles (up to
2 pcs);
- KAB-500 guided
aerial bombs (up to
4 pcs).
The fighter’s weapon control system integrates three
sighting systems: an airborne radar, an optical locator,
and a helmet-mounted target designator.
In November 1997, a new version of the aircraft,
designated MiG-29SMT, entered flight tests.
The MiG-29SMT is a long-range multifunctional fight-
er capable of using the entire range of Russian and
foreign-made airborne weapons.
The MiG-29SMT features the following basic innova-
tions:
- a modernized crew cockpit furnished with up-to-date
multifunctional liquid-crystal displays and control
panels;
- a increased flight range owing to additional internal
fuel tanks;
- an updated airborne radar with a ground-mapping
mode, which considerably increases the effectiveness
of air operations against ground targets;
- new open architecture of an onboard equipment
complex;
- a digital computer boasting extended capabilities.
The inventory of guided weapons intended for defeating
ground and sea targets has been extended owing to:
- active radar-homing antiship missiles;
- antiradar missiles;
- laser-guided missiles and bombs, provided an optical
laser equipment pod is suspended.
With the modernization carried out, the fighter’s
combat effectiveness increases more than three
times and its operating cost decreases 40 percent.
Owing to the all-round modernization of the MiG-29UB
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312
PART 2 2
FIGHTERS
GROUP 15 AIRCRAFT AND AIRFRAME
STRUCTURAL COMPONENTS
Class 1510 Aircraft, Fixed Wing
15 ! !
" #$ ! " %##$
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combat trainer, a two-seat multifunctional fighter, des-
ignated MiG-29UBT, was developed to fly combat and
training missions. The MiG-29UBT may be equipped
with a millimetric- or centimetric-wave band airborne
radar.
The MiG-29K is a ship-based multifunctional fighter
designed to execute naval force air defense mis-
sions and defeat surface and ground targets by
high-precision guided weapons by day and night and
in all-weather conditions. The fighter is equipped
with an up-to-date missile complex and weapon con-
trol/guidance systems ensuring the effective execu-
tion of combat missions. The MiG-29K was success-
fully flight-tested on the Admiral Kuznetsov aircraft
carrier.
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Basic Characteristics
Crew 1
Weight, kg:
takeoff, normal/maximum 15,000/18,000
fuel 4,300
Maximum flight speed, km/h:
near ground 1,500
at height 2,400
Service ceiling, m 18,000
Flight range, km:
near ground 700
at height without/with external fuel tank 1,500/2,100
Maximum operational g-load, g 9
Aircraft overall dimensions
(length x height x wing span), m 17.3 x 4.7 x 11.4
Minimum takeoff/landing run, m 250/600
Engine type, number x thrust, kgf RD-33, 2 x 8,300
313
PART 2 2
FIGHTERS
GROUP 15 AIRCRAFT AND AIRFRAME
STRUCTURAL COMPONENTS
Class 1510 Aircraft, Fixed Wing
15 ! !
" #$ ! " %##$
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MiG-21-93 LIGHTWEIGHT FRONT-LINE FIGHTER
The MiG-21-93 is designed to destroy air targets by day
and night, in VFR and IFR weather conditions, and also
defeat ground targets with unguided and guided
weapons.
The aircraft is a derivative of the MiG-21bis fighter, the
last series version of the MiG-21 aircraft family.
The MiG-21-93 is equipped with Kopyo-21I weapon con-
trol system, comprising:
- Kopyo (Spear) small-size multifunctional coherent
pulse-Doppler radar developed using the technology of
the RLPK-29M radar;
- airborne computer;
- data display system;
- helmet-mounted target designator;
- navigation system.
The Kopyo radar enables the pilot to guide missiles
to target forward and aft hemispheres and against
earth background, detecting targets at altitudes of up
to 30 m.
To deliver close air combat, provision is made for a "ver-
tical" operating mode. The radar enables the pilot to
simultaneously detect and track eight air targets and
attack two of them.
Kopyo detects air targets at a range of 45 km. It can
operate in the aerial mapping mode that enables the pilot
to conduct terrain reconnaissance, recognize large
radiocontrast ground/surface targets and destroy them
with unguided and guided weapons, including Kh-31A
air-to-ship missiles. To defeat radiating targets by
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314
PART 2 2
FIGHTERS
GROUP 15 AIRCRAFT AND AIRFRAME
STRUCTURAL COMPONENTS
Class 1510 Aircraft, Fixed Wing
15 ! !
" #$ ! " %##$
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M(^,-(*T i-31L T i-25bL O( )(*+',-, ]M,NS)*+-M,O( S)-
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mL-21.
Kh-31P and Kh-25MP missiles, the aircraft is provided
with target designation equipment.
To protect the aircraft against air-to-air and ground-to-
air portable air defense missiles, type Stinger, with IR
homing heads, the aircraft is equipped with BVP-21 chaff
dispensers.
Basic Characteristics
Crew 1
Weight, kg:
normal takeoff 8,800
fuel 2,390
Operational flight range
(without external fuel tanks), km 1,210 - 1,400
Maximum flight speed, km/h:
near ground 1,300
at altitude 2,175
Service ceiling, m 17,500
Maximum operational g-load 8.5
Maximum rate of climb, m/s 220 - 290
Armament:
air-to-air missiles four RVV-AE or R-73E
two R-27R1 or R-27T1)
six R-60M
air-to-surface missiles one Kh-31A or Kh-31P
two Kh-25MP
airborne guided bombs two KAB-500Kr (FAE)
unguided aircraft rockets S-8, S-24
air bombs up to ten AB-100
four AB-250
two AB-500
Built-in gun mount Gsh-23L
Ammunition load, rds 200
Aircraft dimensions
(length x height x wing span), m 15.76 x 4.5 x 7.15
Engine type and thrust, kgf R-25-300 X 7,100*
*at emergency power setting 9,900
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315
PART 2 2
FIGHTERS
GROUP 15 AIRCRAFT AND AIRFRAME
STRUCTURAL COMPONENTS
Class 1510 Aircraft, Fixed Wing
15 ! !
" #$ ! " %##$
&'()) 1510 (*+',-.
Basic Characteristics
Crew 1
Normal takeoff weight, kg 14,700
Operational flight range without external fuel tanks, km 1,950
Service ceiling, m 18,500
Maximum rate of climb, m/s 230 - 240
Armament complement:
2 x R-27, 4 x RVV-AE, 4 x R-73E, 6 x K-60 air-to-air missiles;
2 x Kh-31A*, 2 x Kh-35*, 2 x Kh-31P**, 2 x Kh-29T**, 2 x Kh-29L air-to-
surface missiles;
4 x KAB-500KR*, 4 x KAB-500L guided bombs;
S-8, S-13, S-24 unguided rockets;
up to four FAB-500, FAB-250 aerial bombs
Type of built-in gun mount
GSh-23L
Ammunition load, rds 260
Overall dimensions (length x height x wing span), m 16.7 x 5.77 x 7.8/14.0
Engine type, thrust, kgf R-35-300, 13,000
* with new radar
** with L-150 equipment
MiG-23-98 LIGHTWEIGHT FRONT-LINE FIGHTER
The Mig-23-98 is designed to defeat air targets in the
daytime and at night, in VFR and IFR weather condi-
tions, and also destroy ground and surface targets with
unguided and guided weapons.
The aircraft is developed from the production versions
of the MiG-23MLD frontal fighter and the MiG-23P
interceptor using equipment and armament unified for
other MiG fighters.
At customer request, the fighter can be equipped with a
new multifunction multichannel pulse-Doppler radar,
enabling the pilot to use R-73, RVV-AE and R-27 air-to-
air missiles; perform the target designation for Kh-31A
and Kh-35 air-to-ship missiles; and detect pinpoint tar-
gets. Alternatively, the Sapfir-23 modernized radar may
be used to enable the crew to employ the R-73 and
RVV-AE air-to-air missiles, as well as the R-24R, R-23
and R-60 standard missiles.
The aircraft is equipped with an airborne digital com-
puter and a GPS receiver in both radar versions. In the
new radar version, the fighter is furnished with an iner-
tial flight navigation system and a multifunction display.
The MiG-23-98 can additionally be equipped with:
- helmet-mounted target designator;
- new ECM equipment (a radar threat warning station,
an active jammer, and a thermal decoy dispenser);
- target designator for air-to-radar missiles;
- IFF and ATC systems and communications facilities
corresponding to Western standards;
- Karat-B data analysis and recording system;
- video recording equipment;
- flight mission input system;
- sighting and reconnaissance equipment pods;
- armament versions incorporating Kh-29T (TE) and
KAB-500KR TV-guided weapons, as well as Kh-29L and
KAB-500L laser-guided weapons (with a suspended
sighting equipment pod).
Other modification versions can also be considered,
including the use of Western avionics and extending
the fighter’s service life.
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W+'\,\. ^(d+-. W+ W^+c',\Vt ',-\+`+ ^,)h^)(.
316
PART 2 2
FIGHTERS
GROUP 15 AIRCRAFT AND AIRFRAME
STRUCTURAL COMPONENTS
Class 1510 Aircraft, Fixed Wing
15 ! !
" #$ ! " %##$
'()** 1510 )+,(-./
MiG-31 INTERCEPTOR-FIGHTER
The MiG-31 is intended to intercept aerial targets in VFR and
IFR weather conditions, in the daytime and at night,
autonomously and in interceptor groups, in continuous and dis-
continuous fields of control and guidance commands, irrespec-
tive of the target’s defensive maneuver and jamming counter-
measures.
Its combat effectiveness is ensured owing to:
- a wide range of airspeeds and altitudes of intercepted targets;
- semi-autonomous actions in discontinuous or one-time target
data environment;
- capability to simultaneously track several targets and launch
all missiles in one attack during mass air raids of hostile aircraft
and cruise missiles;
- group actions involving the exchange of data and mutual coor-
dinates and distribution of targets between the group intercep-
tors or interceptor groups by commands of the group leader;
- capability of long-endurance air patrolling with subsequent
target interception.
The MiG-31 aircraft weaponry comprises four radar-homing
(R-33E) and four infrared-homing missiles and a built-in gun
mount.
Several interceptor-fighter modifications, such as MiG-31E
(export version) and MiG-31B, were developed from the
MiG-31 baseline aircraft.
The MiG-31B interceptor-fighter features extended combat
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317
PART 2 2
FIGHTERS
GROUP 15 AIRCRAFT AND AIRFRAME
STRUCTURAL COMPONENTS
Class 1510 Aircraft, Fixed Wing
15 ! !
" #$ ! " %##$
'()** 1510 )+,(-./
Basic Characteristics
Crew 2
Takeoff weight, kg:
normal 36,800
maximum 50,000
Maximum flight speed, km/h:
near ground 1,500
at height 3,000
Time to climb 18 km, min 7.9
Interception line, km:
at an altitude of 19 km and M = 2.35 720
at an altitude of 10 km and M = 0.8,
without/with in-flight refueling 1,450/2,250*
Ferry range, km 3,000
Service ceiling, m 20,000
Airfield category Second
Maximum combat load, kg 8,000**
Overall dimensions (length x height x wing span), m 22.69 x 6.15 x 13.46
Engine type, number x thrust, kgf D-30F6, 2 x 15,500
*for MiG-31B (BM)
**for MiG-31BM
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capabilities due to equipping the air-
craft with an in-flight refueling sys-
tem, additional missile armament,
long-range radio navigation system
and additional equipment enabling
the crew to fulfill new tasks.
The MiG-31s, reequipped during
overhaul to the level of the
MiG-31B version, are designated
MiG-31BS.
The MiG-31B became the baseline
aircraft for developing the MiG-31BM
(export version MiG-31FE) multifunc-
tion aircraft capable of engaging aer-
ial and ground/surface targets.
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318
PART 2 2
ATTACK AIRCRAFT
GROUP 15 AIRCRAFT AND AIRFRAME
STRUCTURAL COMPONENTS
Class 1510 Aircraft, Fixed Wing
15 ! !
" #$ ! " %##$
&'(( 1510 )'*+&,-.
&#-(&#$"% )-25
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«&,2-/)».
Su-25 ATTACK AIRCRAFT
The Su-25 attack aircraft is intended to provide direct air
support for troops, defeat multiple and individual small-size
ground targets, carry out aerial mine-laying and engage
low-speed aerial targets in visual conditions, by day and
night, in severe enemy fire opposition environment.
The Su-25 features high combat survivability owing to the
use of an all-welded titanium-armor cockpit and an
armored windscreen, fuel tanks with polyurethane foam,
fire protection of engine compartments, damage-resistant
structures for load-bearing elements, armor plating of vital
units and systems, as well as reinforced fire-resistant
control rods capable of remaining intact even when hit by
12.7mm bullets.
The total weight of combat survivability enhancing assets
is 1,100 kg.
The Su-25’s onboard equipment comprises:
- communications facilities;
- an IFF transponder;
- ECM equipment, including an operating radar detection
set, an active jammer and a flare decoy dispenser;
- an integrated navigation and aiming system, comprising
the ASP-17BTs-8 gun/bomb sight, laser range finder and
Klen-PS target designator.
The aircraft weapons are suspended at ten external-store
hardpoints and comprise:
- air-to-surface laser-guided missiles (2 - 4 pcs);
- up to 500-kg size aerial bombs weighing up to 4,000 kg;
- unguided rockets (up to 8 rocket pods);
- up to four flexible gun pods;
- two air-to-air short-range missiles.
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6+17,(:; :+2-,82,0'>.
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)<-25 ; *2+=+C,&,7+8 )<-25 ()<-39).
319
PART 2 2
ATTACK AIRCRAFT
GROUP 15 AIRCRAFT AND AIRFRAME
STRUCTURAL COMPONENTS
Class 1510 Aircraft, Fixed Wing
15 ! !
" #$ ! " %##$
&'(( 1510 )'*+&,-.
The 30mm built-in gun with a fire rate of 3,000 rounds per
minute and an ammunition load of 250 rounds.
To operate the aircraft from unequipped airfields, provi-
sion is made for a self-contained maintenance package
arranged in four pods carried on external-store hard-
points.
The aircraft high maneuverability enables the crew to hit
targets from the first run and effectively use a terrain relief
to break off an attack.
The Su-25UB two-seat combat trainer, Su-25T antitank
and Su-25TM (Su-39) multirole aircraft versions are devel-
oped from the baseline aircraft.
Basic Characteristics
Crew 1
Takeoff weight, kg:
normal 14,500
maximum 16,500
Weight, kg:
combat load, kg 4,340
internal tank fuel 3,000
Maximum near-ground flight speed, km/h 950
Flight range, km:
operational, near ground,
without external fuel tanks 495
ferry 1,950
Takeoff run
on concrete/unpaved runway, m 550/600
Landing roll
on concrete/unpaved runway, m 600/750
Maximum operational g-load, g 6.5
Overall dimensions
(length x height x wing span), m 15.53 x 4.8 x 14.36
Engine type, number x thrust, kgf R95Sh, 2 x 4,100
#567869: ;<=<>?:=@5?@>@
r:;6'9 1
3&,-2'5 *'((', :=:
2+0*'&D2'5 14500
*':(;*'&D2'5 16500
'((', :=:
@+,7+8 2'=0<3:; 4340
-+6&;7' 7+ 72<-0,22;> @':'> 3000
':(;*'&D2'5 (:+0+(-D 6+&,-' < 3,*&;, :*/4 950
j'&D2+(-D 6+&,-', :*:
60':-;4,(:'5 < 3,*&;
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( 6+17,(2.*; -+6&;72.*; @':'*; 640
6,0,=+2+42'5 1950
j&;2', *:
0'3@,=' 2' @,-+22+8 ///2' =0<2-+7+8 // 550/600
60+@,=' 2' @,-+22+8 ///2' =0<2-+7+8 // 600/750
':(;*'&D2'5 J:(6&<'-'C;+22'5 6,0,=0<3:', ,1. 6,5
s'@'0;-2., 0'3*,0.
(1&;2' > 7.(+-' > 0'3*'> :0.&'), * 15,53 > 4,8 > 14,36
'0:' 17;='-,&5, :+&;4,(-7+ > -5=', :=( 95, 2 > 4100
320
PART 2 2
ATTACK AIRCRAFT
GROUP 15 AIRCRAFT AND AIRFRAME
STRUCTURAL COMPONENTS
Class 1510 Aircraft, Fixed Wing
15 ! !
" #$ ! " %##$
&'(( 1510 )'*+&,-.
Su-39 ALL-WEATHER MULTIFUNCTIONAL
ATTACK AIRCRAFT
The Su-39 attack aircraft is designed to defeat ground,
sea and aerial targets by high-precision weapons in the
daytime and at night, in VFR and IFR weather conditions
and in the enemy air defense opposition environment.
The Vikhr antitank guided missiles (up to 16 pcs) are the
Su-39’s main weapons capable of defeating at a range
of 10 km, a moving battle tank with an armor of up to 1
m thick, boat-type sea targets, and aerial targets, such
as armored combat helicopters and heavy airplanes.
The Su-39 can also be equipped with other state-of-the-
art air-to-surface, air-to-air and air-to-radar high-preci-
sion weapons, 85mm - 250mm unguided rockets, and
up to 500-kg aerial bombs with a total weight of up to
5,000 kg. The aircraft is provided with a 30mm gun
mount.
To achieve high effectiveness of combat missions, the
aircraft is equipped with a flight navigation/fire control
complex and an airborne electronic warfare (EW)
system.
The flight navigation/fire control complex comprises:
- weapon control system enabling the crew to employ
two different weapons in one attack delivered from level
flight, pitch-down and pitch-up;
- Shkval-M automatic day/night optronic complex, with a
23-fold target magnifying optical channel and a system
for target search, detection, identification, tracking and
designation, which ensures the use of all types of guid-
ed and unguided weapons against ground, surface and
aerial targets;
- Kopyo-25 fire control radar intended for employing the
air-to-air and air-to-surface missiles, including those
used against sea targets. The radar features a ground-
mapping mode;
- flight navigation equipment ensuring a target approach
in the automatic operation mode.
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