Каталог - Оружие России 2000 c82-795
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342
PART 2 2
COMBAT HELICOPTERS
GROUP 15 AIRCRAFT AND AIRFRAME
STRUCTURAL COMPONENTS
Class 1520 Aircraft, Rotary Wing
15 ! !
" #$ ! " %##$
+,-.. 1520 /012,/13
Ka-50 BLACK SHARK COMBAT HELICOPTER
The Ka-50 is intended to defeat armored materiel, low-
speed aerial targets, and manpower on the battlefield.
The helicopter features a coaxial configuration. It is
equipped with retractable landing gear. Owing to its
small dimensions, streamlined configuration, and
engine power reserve, the helicopter is able to perform
energetic maneuvers, including nontypical ones, such
as a flat (pedal-assisted) turn. This increases the first-
run weapon employment effectiveness and ensures an
advantage in a duel situation.
The Ka-50 is provided with up-to-date combat surviv-
ability enhancing facilities, including the crew cockpit
armoring. The helicopter is equipped with an emergency
crew escape system involving the K-37 ejection seat that
enables the pilot to abandon the flying machine through-
out the entire flight altitude and speed envelope.
High-precision Vikhr ATGMs, a 30mm rapid-firing flexi-
ble 2A42 gun mount with an ammunition load of 460
rounds, and S-8 and S-13 unguided rockets constitute
the Ka-50’s main armament system. The Igla-V guided
missiles, the gun mount, and the Vikhr ATGMs can be
used to defeat aerial targets.
The following weapons can be suspended at four
underwing hardpoints:
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343
PART 2 2
COMBAT HELICOPTERS
GROUP 15 AIRCRAFT AND AIRFRAME
STRUCTURAL COMPONENTS
Class 1520 Aircraft, Rotary Wing
15 ! !
" #$ ! " %##$
+,-.. 1520 /012,/13
- up to 12 Vikhr ATGMs;
- up to 80 S-8 unguided rockets;
- up to ten S-13 unguided rockets;
- up to four Igla-V guided missiles;
- 23mm gun mount pods;
- various aerial bombs.
The total weight of weapons carried on the underwing
hardpoints is 2,300 kg.
ECM equipment is arranged in pods at wingtips.
The heliborne avionics system enables the crew to per-
form flight control and air navigation round-the clock at
any time of the year. The surveillance and fire control
systems, including TV, laser and thermal imaging
equipment, enable the pilot to detect and defeat tar-
gets in the daytime and at night.
The surveillance and fire control systems of the Ka-50’s
night version are additionally equipped with a TV chan-
nel. For night flight, the pilot is provided with night
vision goggles.
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Basic Characteristics
Crew 1
Weight, kg:
takeoff, normal/maximum 9,800/10,800
maximum combat load 2,500
Flight speed, km/h:
maximum (when diving) 390
cruising 270
Ceiling, m:
hovering 4,000
service 5,500
Maximum vertical acceleration, g 3.5
Operational flight range, km:
with normal takeoff weight 520
with additional fuel tanks 1,100
Airframe dimensions (length x height x width), m 14.2 x 4.93 x 7.34
Rotor diameter, m 14.5
Engine type, number x power, hp TV3-117VMA, 2 x 2,200
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344
PART 2 2
COMBAT HELICOPTERS
GROUP 15 AIRCRAFT AND AIRFRAME
STRUCTURAL COMPONENTS
Class 1520 Aircraft, Rotary Wing
15 ! !
" #$ ! " %##$
+,-.. 1520 /012,/13
Ka-52 ALLIGATOR
ALL-WEATHER MULTIROLE COMBAT HELICOPTER
The Ka-52 is intended to defeat armor materiel, low-speed
aerial targets, as well as uncovered and covered manpower in
the daytime and at night, in VFR and IFR weather conditions.
The two-seat Ka-52 is capable of carrying out group combat
actions, including those involving a combined air strength
(Ka-52 and Ka-50 combat helicopters).
The crewmembers are
accommodated side by
side in a common cock-
pit and each crewmem-
ber can fly the heli-
copter and control all its
systems. The helicopter
is equipped with all
weapons carried by the
Ka-50, including the
Vikhr ATGMs and the
Igla-V guided missiles.
The two-man crew
makes it possible to
extend an array of com-
bat missions and Ka-52
employment conditions.
The Ka-52 is equipped
with a new integral mul-
tifunctional avionics
complex incorporating
passive/active surveil-
lance and sighting sys-
tems. The complex is
intended for piloting, air
navigation and weapon
control.
The helicopter can be
used for training pur-
poses.
In terms of its airframe
and systems, the
Ka-52 is identical by 85
percent with the Ka-50
helicopter, which facili-
tates full-scale production and decreases operation costs. The
Ka-50-2 helicopter version with a tandem crew seating config-
uration is currently being developed from the Ka-52.
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Basic Characteristics
Crew 2
Normal takeoff weight, kg 10,400
Flight speed, km/h:
level flight, maximum 310
when diving 350
Ceiling, m:
hovering 3,600
service 5,500
Maximum vertical acceleration, g 3.0
Service range with normal takeoff weight, km 520
Airframe dimensions (length x height x width), m 13.53 x 4.95 x 7.34
Rotor diameter, m 14.5
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345
PART 2 2
COMBAT-TRANSPORT HELICOPTERS -
GROUP 15 AIRCRAFT AND AIRFRAME
STRUCTURAL COMPONENTS
Class 1520 Aircraft, Rotary Wing
15 ! !
" #$ ! " %##$
12344 1520 56782579
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Mi-24 (Mi-35, Mi-35M)
COMBAT/TRANSPORT HELICOPTERS
Intended for air support of the ground forces units by fire
at enemy combat equipment (including armor materiel)
and manpower, heliborne assault party landing, as well
as for evacuation of the wounded from a battlefield.
The helicopters are designed around a conventional
single-rotor configuration with a tail rotor and
retractable tricycle nosewheel type landing gear.
The pilot and weapon operator are seated in tandem
cockpits under individual canopies.
The Mi-24’s distinguishing feature is its cabin which
can accommodate eight airlanding troopers.
The helicopter is powered by two TV3-117VMA tur-
boshaft engines with air intakes equipped with dust-
proof devices to protect the powerplant from erosive
wear when operating from unprepared sites. The heli-
copter is furnished with an auxiliary power unit for
autonomous operation.
To enhance the helicopter combat survivability, provi-
sion is made for:
- crew cockpit armoring;
- porous fuel tank filler;
- fuel tank self-sealing covers;
- firefighting equipment;
- infrared suppression exhaust mixer boxes over engine
exhaust ducts;
- redundancy and backup of hydraulic and electric power
sources and main control circuits.
The outboard wing panels are equipped with six hard-
points for weapon suspension.
346
PART 2 2
COMBAT-TRANSPORT HELICOPTERS -
GROUP 15 AIRCRAFT AND AIRFRAME
STRUCTURAL COMPONENTS
Class 1520 Aircraft, Rotary Wing
15 ! !
" #$ ! " %##$
12344 1520 56782579
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- 16 q «73A3», 10 -13;
- 8 q «pG23», 40 -8;
- 8 q «pG23», 10 -13;
- 80 -8;
- 20 -13.
Since the beginning of the Mi-24’s full-scale produc-
tion (1970), the following modifications have been
manufactured:
- Mi-24P, equipped with a 30mm built-in fixed gun
mount;
- Mi-24D (its export version Mi-25), equipped with the
Falanga ATGM system and a 12.7mm built-in flexibly
mounted machine gun;
- Mi-24V (its export version Mi-35), equipped with the
Shturm ATGM system and a 12.7mm built-in flexibly
mounted machine gun;
- Mi-24VP, armed with the Shturm ATGM system and a
23mm built-in flexibly mounted gun with ammunition
load of 470 rounds.
All the Mi-24 family helicopters (including their export
versions) are armed with unguided rockets, podded
machine guns, grenade launchers and guns, and are
equipped with surveillance and aiming, flight control
and navigation, radio communications and other equip-
ment enabling the pilot and pilot-operator to execute
flight control, navigation and sighting missions.
The onboard equipment enables the crew to fly the
helicopter in the daytime and twilight in VFR weather
conditions.
The helicopters can be operated from poorly prepared
natural-surfaced sites virtually in any physical and geo-
graphical environment.
The Mi-24VM version (its export version Mi-35M) fea-
tures the following:
- the helicopter is equipped with a main rotor fitted with
glassfiber blades unified with those of the Mi-28N, a
hub requiring no lubrication, and a low-noise X-shaped
tail rotor;
- the airframe is lightened (the wing is shortened, non-
retractable landing gear is used, etc.);
- the armament system is complemented with the
Ataka air-to-ground and Igla air-to-air missiles;
- the helicopter is additionally equipped with a comput-
er complex and a laser rangefinder.
The updated avionics ensures round-the-clock combat
employment of the Mi-35M helicopter.
The Mi-35M’s armament versions are as follows:
- four Ataka and two Igla missiles, 40 S-8 unguided
rockets;
- 16 Ataka missiles, 40 S-8 unguided rockets;
- 16 Ataka missiles, ten S-13 unguided rockets;
- eight Igla missiles, 40 S-8 unguided rockets;
- eight Igla missiles, ten S-13 unguided rockets;
- 80 S-8 unguided rockets;
- 20 S-13 unguided rockets.
347
PART 2 2
COMBAT-TRANSPORT HELICOPTERS -
GROUP 15 AIRCRAFT AND AIRFRAME
STRUCTURAL COMPONENTS
Class 1520 Aircraft, Rotary Wing
15 ! !
" #$ ! " %##$
12344 1520 56782579
Basic Characteriatics
Mi-35 (Mi-35M)
Crew 2
Takeoff weight, kg:
normal 11,100 (10,800)
maximum 11,500 (11,500)
Main rotor diameter, m 17.2
Flight range, km:
operational (with normal takeoff weight) 450 (500)
ferry 1,020 (1,085)
Flight speed, km/h:
maximum 320 (310 to 330)
cruising 270 (260)
Ceiling, m:
hovering 2,200 (3,100)
service 4,500 (5,750)
Overall dimensions (length D height D width), m:
cabin for airlanding troopers 2.5 D 1.2 D 1.45
helicopter (less main rotor) 18.6 D 4.8 D 4.4
Engine type, number x power, hp TV3-117VMA, 2 x 2,200
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348
PART 2 2
COMBAT-TRANSPORT HELICOPTERS -
GROUP 15 AIRCRAFT AND AIRFRAME
STRUCTURAL COMPONENTS
Class 1520 Aircraft, Rotary Wing
15 ! !
" #$ ! " %##$
23455 1520 6789368:
Mi-8AMTSh MILITARY TRANSPORT HELICOPTER
The Mi-8AMTSh is one of the latest modifications of the Mi-8
helicopters. The Mi-8AMTSh is equipped with Shturm-V and
Igla-V high-precision guided missile systems which make it
possible to effectively use the helicopter for defeating armor
materiel (including modern battle tanks provided with explosive
reactive armor), fortified points, and aerial targets in addition to
the execution of traditional missions involving an airlift of heli-
borne assault forces, transportation of cargoes, as well as
evacuation and search/rescue operations.
The Shturm-V system uses the Ataka supersonic missile
(previously manufactured Shturm missiles may be used)
that allows defeating armor materiel (by a hollow-charge
warhead), aerial targets (by a fragmentation warhead),
manpower and lightly armored combat materiel (by a
high-explosive warhead). The Igla-V missile system is
intended for aerial target combating.
In addition to the guided weapons, S-8 unguided rocket pods
or GSh-23L gun pods may be suspended at special hard-
points.
The 7.62mm PKT machine guns are installed in the nose and
rear fuselage sections.
Gun pivots installed at the doorway and near the windows
enable the heliborne troopers to employ their organic
weapons in flight.
The combat survivability of the helicopter is ensured by armor
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349
PART 2 2
COMBAT-TRANSPORT HELICOPTERS -
GROUP 15 AIRCRAFT AND AIRFRAME
STRUCTURAL COMPONENTS
Class 1520 Aircraft, Rotary Wing
15 ! !
" #$ ! " %##$
23455 1520 6789368:
protection of the crew cabin and vital units, by infrared sup-
pression exhaust mixer boxes over engine exhaust ducts
which considerably decrease an infrared signature of the heli-
copter, an IR-decoy dispensing system, fuel tank self-sealing
covers and polyurethane foam protection intended to prevent
fuel explosion and leakage in case of combat damage.
Twelve stretchers for the wounded can be arranged in the
cargo cabin.
The helicopter's main armament versions are as follows:
- 80 S-8 unguided rockets;
- 40 S-8 unguided rockets, two GSh-23L gun pods with an
ammunition load of 250 rounds per gun;
- eight Ataka guided missiles, 40 S-8 unguided rockets;
- eight Ataka guided missiles, two GSh-23L gun pods with an
ammunition load of 250 rounds per gun;
- four Igla guided missiles, 40 S-8 unguided rockets;
- eight Ataka guided missiles, four Igla guided missiles.
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Basic Characteristics
Crew 3
Takeoff weight, kg:
normal 11,100
maximum 13,000
Fuel capacity, kg:
main fuel tanks 1,930
auxiliary fuel tanks 1,388
Cargo-carrying capacity, kg:
in cargo cabin 4,000
on slings 4,000
Flight speed, km/h:
maximum 250
cruising 230
Ceiling, m:
hovering 3,980
service 6,000
Flight range, km:
operational (without auxiliary fuel tanks) 580
ferry 1,250
Overall dimensions (length x height x width), m:
helicopter 18.4 x 6.4 x 4.8
cargo cabin 5.3 x 2.3 x 1.8
Main rotor diameter, m 21.3
Engine type, number x power, hp TV3-117VM, 2 x 2,200
350
PART 2 2
MULTIROLE HELICOPTERS
GROUP 15 AIRCRAFT AND AIRFRAME
STRUCTURAL COMPONENTS
Class 1520 Aircraft, Rotary Wing
15 ! !
" #$ ! " %##$
-./00 1520 1234.135
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R>/?132 810FN1E4 <>83/, ? 13,5
/2=/ 7<>E/31.;, =4.-<4 C ?4N8403@, ..0. R-600, 2 C 1300
Basic Characteristics
Crew 1 - 2
Maximum weight, kg:
takeoff 6,500
in cargo hold/slung cargo 2,000/2,750
Flight speed, km/h:
maximum 300
cruising 265
Ceiling, m:
hovering 2,100
service 5,150
Service range
without external fuel tanks, km 700
Overall dimensions (length x height x width), m:
airframe 13.47 x 4.6 x 3.0
cargo/passenger compartment 3.4 x 1.30 x 1.78
Main rotor diameter, m 13.5
Engine type, number C power, hp RD-600, 2 x 1,300
Ka-60 SWALLOW MULTIROLE HELICOPTER
The Ka-60 is intended for air delivery in the daytime and at
night, in VFR and IFR weather conditions of air landing troops,
weapons and ammunition to combat areas, evacuation of the
wounded, air patrolling with takeoff from a ship-based helipad,
and flight personnel training. The helicopter features a five-
blade single main rotor and multi-bladed steering rotor con-
figuration. The airframe has a streamlined shape and is pro-
vided with large openings for sliding doors on both sides.
Power-intensive tricycle landing gear and energy-absorbent
seats ensure safety for the crew and air landing troops in
emergency landing. Polymeric composite materials are wide-
ly used in the helicopter structure.
To enhance its combat survivability, all main systems and
units of the Ka-60 are redundant and spaced apart on either
side of the fuselage.
The rotor blades
remain serviceable
even when hit by
several small-arms
bullets, while the
control system tie
rods and transmis-
sion shafts remain
intact even when hit
by the 12.7mm bul-
lets. The fuel tanks
are provided with
porous fillers.
The onboard avionics
complement de-
pends on the heli-
copter version. The
troop-carrying heli-
copter is the basic
version.
351
PART 2 2
MILITARY TRANSPORT
HELICOPTERS
-
GROUP 15 AIRCRAFT AND AIRFRAME
STRUCTURAL COMPONENTS
Class 1520 Aircraft, Rotary Wing
15 ! !
" #$ ! " %##$
/0122 1520 34560357
Mi-26 HEAVY MILITARY
TRANSPORT HELICOPTER
The Mi-26 is designed for carrying troops, combat materiel,
cargoes in its cargo hold and on slings, as well as for air-
landing of personnel and combat equipment in a wide range
of weather conditions and at any time of the day.
The Mi-26 is the world’s largest cargo-carrying serially-pro-
duced helicopter capable of airlifting a wide range of combat
equipment in its cargo hold. In the troop-carrying version, it
can carry up to 82 air landing troopers.
The ambulance version is furnished with medical personnel
workstations, respective equipment and fasteners for 60
stretchers.
The onboard equipment enables the crew to perform flight
and landing in adverse weather conditions.
For cargo loading/unloading, the helicopter is equipped with
two winches with a load-lifting capacity of 1,500 kg each and
an electric telpher with a cargo-carrying capacity of 5,000 kg.
The cargo handling operations can be monitored by means of
an onboard TV camera which is also used to monitor slung
payloads.
To enhance combat survivability of the Mi-26, provision is
made for detachable armor plating, porous fuel tank fillers,
firefighting equipment, as well as backup and redundancy of
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