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LAS-XF2 'Foiler'

http://www.robotechresearch.com/rpg/vehicles/ebsis/sukhoi_s_37/s37_3.jpg

The XF2 is produced by Lasatanian Aeronautical Industries under licence from the Sukhoi Design Bureau, Russia, and offers Fifth-generation fighter capability unsurpassed by any fighter in service.

The XF2 features forward-swept wings, which promises a range of benefits in aerodynamics at subsonic speeds and at high angles of attack. The forward-swept wing, which enables the aircraft to increase its range and its manoeuvrability at high altitude, makes extensive use of composite materials. The aircraft has large canards mounted on the intake side, close to the leading edge of the wing. The vertical stabilizers are canted slightly outward, and two large auxiliary intake doors are visible on the center fuselage section.

Any nation wishing to discuss purchasing the foiler please contact LasProd. Export of this aircraft is planned eventually though strategic partners can exhange technology for deliveries of this aircraft.

LAS-XF2 'Foiler'

cost: $80m

Specifications:
Wingspan: 15.16 m - 16.7 m
Length overall: 22.2 m - 22.6 m
Height overall 6.36 m - 6.40 m
Weight empty, equipped : 24,000 kg (52,910 lb) -- 26000 kg (57,320 lb)
Max T-O weight : 34,000 kg (74,960 lb)
Engines: 2 Perm Aviadvigatel D-30F6 (34,170 lbst), or
2 Saturn/Lyul'ka AL-37FU afterburning 142.2 kN (31,966 lb st) with afterburning
thrust-vectoring in pitch -20o to 20o at 30o per second
Max level speed at height : 2,500km/h (1,350 knots)
Max level speed at S/L : 1,400km/h (756 knots)
Service ceiling : 18,000 m (59,050 ft)
Range with max fuel at height : 1,782 nm (3,300 km/2,050 miles)
Number of hardpoints: 14: 2 wingtip, 6-8 underwing, 6-4 conformal underfuselage
Air-to-air : R-77, R-77PD, R-73, K-74
Air-to-surface: X-29T, X-29L, X-59M, X-31P, X-31A, KAB-500, KAB-1500
Crew: 1

LAS-XF3 'Firestorm'


http://www.globalsecurity.org/military/world/russia/images/i42-001.jpg

The new Lasatanian Aeronautical Industries LAS-XF3 was unveiled publicly on 12 January 1999. The project has been under development since 1986, is variously designated the 1.42, the 1.44, I-42 and I-44 - the "MiG-35" and "MiG-39" designations are informally applied by some observers. 1-42 and 1-44 believed to be designations of the two prototypes, with the 1.44 used for the flight-test airframe(s). This multi-functional front-line fifth-generation fighter was initially developed by the MIG [Mikoyan & Gurevich] aviation scientific and production complex of the MAPO military-industrial corporation, Russia.

The first prototype was delivered early in 1994, and in December 1884 taxi-tests were conducted following which further work was suspended due to a shortage of funds. The 35-ton fighter features a single under-fuselage air intake with two AL41F engines of 20 tons thrust each, and a top speed of over 2,500 km/h. The twin-tail "duck" planform features an all-moving canard-type foreplane with a wingspan of about 15 meters and a length of about 20 meters.

Following the failure of the Russian government to provide sufficient funding for the project, Lasatanian Aeronautical Industries stepped in and took over development of the fighter in a joint venture with MiG.

Production of the reclassified LAS-XF3 Firestorm commenced in 2002 and delivery of the aircraft to squadrons in Lasatania commenced in June 2004, with the 1st Air Guards becoming the first squadron equipped with the fighter.

Lasatanian Aviation Industries claims the new fighter would be able to outperform the F-22 Raptor, the most advanced US air-superiority fighter. Although the primary mission of the MFI is air-superiority, unlike the F-22 the MFI is also capable of performing strike mission, and thus in both conception and configuration is more directly comparable to the similar multi-role EFA2000 Eurofighter. Like the American F-22, the MFI has a thrust vectoring system that allows it to make sharp turns. It also has similar stealth capabilities, with the canard, wing and fuselage structures incorporating carbon-fiber and polymer composite materials. Other stealth features include radar-absorbing covering, screening of radar-visible structure elements, and reduced heat signature. The fifth-generation pulse-doppler radar has a phased-array andtenna with electronic scanning to simultaneously attack over 20 targets. The aircraft can carry long-range air-to-air and air-to-surface guided missiles, and it is armed with a 30-mm cannon.


LAI-XF3 'Firestorm'

http://globalsecurity.org/military/world/russia/images/i42-012.jpg

Prime contractor: Lasatanian Aeronautical Industries (sourced from MiG-MAPO)

Nation of origin: Russia/Lasatania

Function: Multi-role fighter

Crew: 1

Cost: $80m

First: Flight 1999

In-service year: 2004

Engine: Two Lyulka AL-41F vectored-thrust afterburning turbofans, 39,340 lb thrust each

Wing span: 15 m / 49 ft 3 in

Length: 19 m / 62 ft 4 in

Height: 6 m / 19 ft 8 in

Canard span 5 m / 16 ft 5 in

Weight (approx.) 33,069 lb empty /
44,092 lb max. take off

Ceiling N/A

Speed @ altitude: In excess of 2,448 km/h / 1,521 mph

@ supercruise: In excess of 1,224 km/h / 760 mph
Range: 4,500 KM

Armament: One GSh-30-1 30mm cannon, plus up to 18,075 lb including R-73/R-77 AAMs, ASMs, bombs, rockets, drop tanks, and ECM pods carried on fourteen external points

http://afbase.com/img/acdata/fighter/mig-35/mig35-02.jpg

LAS-F2 "Freefall" [Mig-21BIS / Fishbed-N]


http://www.highgallery.com/ForeignAircraftCockpits-c--mig-21.jpg


Seeking to provide a low-cost air defence solution for emerging nations and client states, Lasatanian Aeronautical Industries has commenced production of a MiG-21 variant, the LAS-F2 'Freefall'. The LAI version shall feature enhanced avionics and control systems.

Truly one of the most remarkable aircraft of the Cold War period and perhaps the most successful aircraft in terms of number built since World War II, the MiG-21 has seen service with some 47 different nations throughout Asia, Africa, the Americas, and Eastern Europe since the late 1950s. The Soviet Air Force requested a short-range interceptor to replace the MiG-17 and MiG-19 fighters in 1953. After experimenting with various wing configurations, the Mikoyan Gurevich design bureau chose a tailed delta configuration which eventually became the MiG-21. The original design was extremely light and maneuverable with exceptional reliability, sortie-rate, and low cost of operation.

Estimated cost: $5m

Description
Manufacturer: Mikoyan-Gurevich OKB / Lasatanian Aviation Industries
Designation: Mig-21
Version: BIS
NATO Code: Fishbed-L/N
Type: Fighter
Crew: Pilot
First Flight: 1972
Specifications
Length: 51' 5.5" 15.00 M
Height: 14' 9" 4.5 M
Wignspan: 23' 5.5" 7.15 M
Wingarea: 247.60 Sq Ft 23.00 Sq M
Empty Weight: 13600 lbs 6050 Kg
Max Weight: 221607lbs 10050 Kg
Propulsion
No. of Engines: 1
Powerplant: Tumansky R-25 turbojet
Thrust (each): 16535 lbs
Performance
Range: 1118 miles 1800.00 Km
Max Speed: 1250 Mph 2050 Km/H Mmax 2.05
Ceiling: 54500 Ft 16000 M


Note: Weapons systems ARE NOT supplied with this aircraft.

Lasatanian Aeronautical Industry's catalog has been augmented with the introduction of the LAS-F6 'Fullback', carrier aircraft. Based on Su-33 airframes and featuring augmented avionics and HUD interface. Interested parties can contact LasProd regarding exports in the usual manner.


LAS-F6 'Fullback'

http://globalsecurity.org/military/world/russia/images/su27k1.jpg

http://www.flyconsult.ch/dsu33p.jpg

The longitudional triplane layout of the LAS-F6 gives it exceptional manouverability, even with heavy loads. The LAS-F6 is intended for fleet air defence (like the F14 is) but is also to have a secondary anti-ship capability. The other attack aircraft to compliment the Su33 on the carrier is a navalised Su35.

Cost: $35m

Power Plant of the LAS-F6
Specifications for the AL-31F Data
Thrust, (sea level, static, dry), (kg) 7 600
Thrust, (sea level, static, after burning), (kg) 12 500
Internal fuel, kg 9 400
In flight refueling provision Present




Dimensions of the LAS-F6
Specification Measurement
Wing Span 14.70 m
Length (excluding nose probe) 21.94 m
Height 6.36 m
Wing surface 62 m2




Weights of the LAS-F6
Aircraft State Weight
Empty Not Avaliable
Normal take-off Not Avaliable
Thrust to weight ratio Not Avaliable
Maximum take-off Not Avaliable
Thrust to weight ratio Not Avaliable




Performance of the LAS-F6
Action Data
Max speed at height Mach 2.165
Take off run with 14 degree ramp 395 ft
Range on internal fuel 1 865 miles




Armament
Number and Category Type
One 30 mm cannon 150 rounds
Up to 10 Air to Air missiles including: R-27 (AA-10 "Alamo")
R-73A (AA-11 "Archer")
R-60 (AA-8 "Aphid")
8 819 lb of air to surface weapons
Same range as the Su27 but with the addition of the Kh-31 (AS-17)

LAS-F7 'Flashback' (SU-15TM 'Flagon F)

http://147.71.210.21/fm4480/chpt6/flagon/flagn_p2.gif

Developed to replace the Su-11 interceptor during the 1960s, the Sukhoi Su-15 first appeared as a scaled-up version of the Su-9/Su-11 family but powered by two engines and utilizing twin side inlets. These design changes freed up space in the new solid nose for a large radar, and powerful engines were installed to insure the Su-15 would fly considerably faster than any known Western aircraft of the time. The first production 'Flagon-A' models featured a mid-mounted cropped delta wing, swept tail surfaces, and a large bubble canopy placed aft well of the conical nose. Later models introduced a "kinked-delta" wing planform of greater span and a more aerodynamic ogival nose. In addition, the electronics, engines, and armaments were continually upgraded so that the Su-15 remained a formidable high-speed interceptor through the 1980s.

The LAS-F7 variant shall have improved radar capability as well as a new Pilot/HUD interface.

Note: Weapons systems are fitted as standard with this aircraft.

Specifications:

HISTORY:
First Flight 30 May 1962
Service Entry 1967


CREW: 1 pilot


AIRFOIL SECTIONS:
Wing Root TsAGI S7s-12
Wing Tip TsAGI S7s-12


DIMENSIONS:
Length 70.25 ft (21.41 m)
Wingspan ('Flagon-A') 28.24 ft (8.62 m)
('Flagon-F') 30.67 ft (9.34 m)
Height 16.50 ft (5.00 m)
Wing Area 394 ft2 (36.6 m2)
Canard Area not applicable


WEIGHTS:
Empty ('Flagon-A') approx. 25,000 lb (11,340 kg)
('Flagon-F') approx. 27,000 lb (12,245 kg)
Typical Load unknown
Max Takeoff ('Flagon-A') approx. 35,275 lb (16,000 kg)
('Flagon-F') approx. 40,000 lb (18,145 kg)
Fuel Capacity internal: unknown
external: unknown
Max Payload: unknown


PROPULSION:
Powerplant two Tumanskii R-13F2-300 afterburning turbojets
Thrust 31,460 lb (139.95 kN)


PERFORMANCE:
Max Level Speed at altitude: 1,385 mph (2,230 km/h) at 36,090 ft (11,000 m), Mach 2.1
at sea level: unknown
Initial Climb Rate 45,000 ft (13,730 m) / min
Service Ceiling 60,700 ft (18,500 m)
Range typical: 780 nm (1,450 km)
ferry: 1,080 nm (2,000 km)
g-Limits unknown


ARMAMENT:
Gun none
Stations six external hardpoints
Air-to-Air Missile typically two R-98M/AA-3 Anab and two R-60/AA-8 Aphid
Air-to-Surface Missile none
Bomb none
Other 23-mm GSh-23L twin-barrel gun pods

Cost: $10M

LAS-F100 'Fistfight'

http://www.military.cz/russia/air/suchoj/Su_9/big/T-43_1.jpg



Seeking to further cement its position as the leading supplier of low-cost air defence solutions, Lasatanian Aeronautical Industries has announced the launch of the LAS-F100 Fistfight interceptor. Based on the Sukhoi Su-9, the Fistfight offers a low cost air defence to nations facing severe financial constraints or developing their air defence systems for the first time. The aircraft can also be used in a training role, whether it be for combat or flight training.

Specifications

Crew one

Role interceptor
air superiority

Armament: missiles
gunpack

Engines 1 * 9060kg Lyulka Al-7F
Wing Span 8.43m
Length 16.70m
Height
Empty Weight 8750kg
Max.Weight
Speed 1915km/h
Ceiling 16800m
Range

Cost: $275,000

Note: armament will be adjusted to buyer's specifications.

http://www.airforce.ru/photogallery/tsvetkov/su-9/ts-9.jpg

LAS-B1 "Bloodstain" (Tu-26 "Backflash")

http://www.futura-dtp.dk/Flysiden/images/Backfire.jpg


DESCRIPTION:
Because the performance of the Tu-22 was far less than designers had hoped for, the Tupolev design bureau extensively modified the design to produce the Tu-22M. The Backfire, as it is known in the West, features swing wings and more powerful engines located within the fuselage rather than on external pods. As a result of these changes, the Tu-22M can reach speeds of Mach 2 at altitude and close to Mach 1 in low level flight. About 300 Backfires were built with the majority going to Naval Aviation units for use as anti-shipping bombers before production ceased in 1993.


The LAS-B1 variant shall feature improved subsonic handling, a new defence awareness system and shall be suitable for the delivery of the new LAS-ASMN-1 'Mildew' Air to Surface, anti-ship missle.


Data below for Tu-22M-3
Last modified 24 May 2001



HISTORY:
First Flight (Tu-22M-0) 1969
(Tu-22M-3) 1977
Service Entry

(Tu-22M-1) 1973
(Tu-22M-3) 1984


CREW: 2 pilots, 1 navigator, 1 weapons systems officer



AIRFOIL SECTIONS:
Wing Root unknown
Wing Tip unknown


DIMENSIONS:
Length 139.31 ft (42.46 m)
Wingspan unswept: 112.48 ft (34.28 m)
swept: 76.46 ft (23.30 m)
Height 36.25 ft (11.05 m)
Wing Area 1,770 ft2 (165.0 m2)
Canard Area not applicable


WEIGHTS:
Empty 119,048 lb (54,000 kg)
Typical Load unknown
Max Takeoff 278,660 lb (126,400 kg) with jet-assisted take-off (JATO) units attached
Fuel Capacity internal: unknown
external: unknown
Max Payload 52,910 lb (24,000 kg)


PROPULSION:
Powerplant two Kuznetsov/ KKBM NK-25 afterburning turbofans
Thrust 110,230 lb (490.4 kN)


PERFORMANCE:
Max Level Speed at altitude: 1,240 mph (2,000 km/h) at 36,090 ft (11,000 m), Mach 1.88
at sea level: 650 mph (1,050 km/h)
Initial Climb Rate unknown
Service Ceiling 43,635 ft (13,300 m)
Range typical: 2,755 nm (5,100 km)
ferry: 4,320 nm (8,000 km)
g-Limits unknown


ARMAMENT:
Gun one or two GSh-23 23-mm twin-barrel cannon in tail (250 rds ea)
Stations one internal weapons bay and two external hardpoints
Air-to-Surface Missile (Tu-22M-2) up to 3 Kh-22/AS-4 ASM
(Tu-22M-3) up to 10 Kh-15P SRAM
Bomb FAB-250, FAB-500, FAB-1500, FAB-3000
Other sea mines


Note: Weapons systems ARE NOT fitted as standard with this aircraft, designated use and weapons systems are at purchasing nations discretion.

COST: $40M

LAS-B2 "Brightstar"

http://repter.adatpark.hu/planepic/tu160-1.jpg


Based on the Tupolev 160, the LAS-B2 “Brightstar” is a multi-mission strategic bomber designed for operations ranging from subsonic speeds and low altitudes to speeds over Mach 1 at high altitudes. The two weapons bays can accommodate different mission-specific loads, including strategic cruise missiles, short-range guided missiles, nuclear and conventional bombs, and mines. Its basic armament of short-range guided missiles and strategic cruise missiles enables it to deliver nuclear strikes to targets with preassigned coordinates.In the future, after the aircraft is equipped with high-precision conventional weapons it may also be used against mobile or tactical targets.

The LAS-B2 “Brightstar” is characterized by low-mounted, swept-back, and tapered, variable geometry wings with large fixed-center section. The variable geometry wings (from 20 degrees up to 65 degrees) allows flight at supersonic and and subsonic speeds. Four LAI-XK22 [turbojet bypass engines with afterburners] of 28,000 kilograms-force power the LAS-B2. The four turbofans, developed by LAI in 1987, are mounted in pairs under the fixed-center section with square intakes and exhausts extending behind the wings’ trailing edges. The fuselage's slim structure is marked by a long, pointed, slightly upturned nose section and a stepped canopy. Tail flats are swept-back, tapered, and mid-mounted on the fin. The tail fin is back-tapered with a square tip and a fairing in the leading edge. The tail cone is located past the tail section. During the design of the aircraft, special attention was paid to reducing its signature. Measures were applied to reduce the signature of the engines to infra-red and radar detectors. Tests of these survivability measures were first tested on a LAS-B1 aircraft in 1980.

As the most powerful combat aircraft of the LAF, the LAS-B2 flies at 2,000 km/hr and can exceed the 2,000 mark with a mission-specific load. The LAS-B2 can climb 60-70 meters per second and reach heights of up 15,000 meters. The bomber can be refueled during flight by IL-78 and ZMS-2 tanker aircraft. The air refueling system consists of a probe and drogue airborne refueling system.

The LAS-B2 “Brightstar” can carry up to 12 Kh-55 long range missiles and Kh-15 short range missiles. The weapons bays can accommodate different loads: carries various bombs: From fee falling nuclear and regular up to 1500 kg bombs. The bomber is not equipped with artillery armament.

The LAS-B2 “Brightstar” is equipped with a combined navigation-and-weapon aiming system, RID; [radar] for detecting targets on the ground and sea at long distances, an optical-electronic bombsight, an automatic terrain-following system, and active and passive radio-electronic warfare systems, as well as a probe-and-drogue airborne refueling system. It is equipped with K-36DM ejection seats. The cockpit instruments are the traditional electromechanical type. The aircraft is controlled with the aid of a central control column. The engine control throttles are located between the pilots' seats. There is a rest area, a toilet, and a cupboard for warming up food.



Soviet Designation
TU-160

Design Bureau
LAI / OKB-156 Tupolev

Manufacturer
Plant Nr. 22 Kazan (TU160) / LAI, Neirsten

Power Plant
Four LAI-XK22 turbojet engines

Thrust
28000 kg each

Length
54.1m

Height
13.1m

Wingspan
35.6m (minimum), 55.7m (maximum)

Wing surface
232 sqm

Speed
2200 km/h (maximum), 1030 km/h (ground)

Ceiling
16000m

Weight (empty)
110000kg

Fuel weight
148000 kg

Maximum take-off weight
275000 kg

Normal load
9000 kg

Maximum load
40000

Range
14000 km (with a load of 9.000kg)

10500 km (with a load of 40.000 kg)

Armament
12 H-55 or 24 H-15 missiles

free falling bombs

Crew 4


Development began
1975 (TU160) / 1998 (LAS-B2)

First Flight
12/19/1981 (TU-160) / 12/07/2000 (LAS-B2)

Series production started
1984 TU160 / 2003 LAS-B2

Date deployed
1987 (TU160) / 2004 (LAS-B2)


UNIT COST: $200M




The LAS-B2 Brightstar in tests

http://www.globalaircraft.org/photos/planephotos/tu-160_4.jpg

http://www.hrvatski-vojnik.hr/hrvatski-vojnik/872002/87_bpictures/HV-87=TU-160=07.jpg

We are pleased to announce the introduction of the new LAS-Xb1 'BlackBear' - a next generation multi-role aircraft produced by Lasatanian Aeronautical Industries.

LAS-XB1 'BlackBear'

http://www.aeronautics.ru/img001/t4ms01a.jpg

In the mid-1990s, the first priority for the LAF was the development of a next generation bomber to replace the LAS-B1. The LAS-XB1 is a long-range supersonic tactical/operational nuclear-capable bomber with built-in stealth technology developed by LAI in conjunction with the Sukhoi Design Bureau. Although its development was officially secret, the LAS-XB1 was reported to be in the prototype stage and ready for flight testing in mid-1996.

The LAS-XB1 project for a high-altitude, high-speed bomber was initiated by the LAF in 1984 and originally intended to enter service in 2003. The LAS-XB1 is comprised of a blended-body fuselage and a swing-wing construction. The design is capable of supercruise at Mach 2, with engines equipped with two-dimensional thrust vectoring nozzles to solve the problem of insufficient area of horizontal control surfaces at high speeds encountered during the development effort.

Type: intermediate-range strike/interdiction aircraft
Powerplants two LAI-STRX12 23,500 kg (51,800 lb) turbofans
Max speed: Mach 2.04
Cruising speed: Mach 2.02
Max altitude: 20,000 m (65,500 ft)
Cruising altitude: 15,000 m (49,000 ft)
Max range: 6,000 km (3,250 nm)
Range with max load: 2,200 km (1,200 nm)
Weight (empty): 32,000 kg (70,500 lb)
MTOW: 85,000 kg (188,000 lb)
Max load: 20,000 kg (44,000 lb)
Wing span (extended): 37 m (121 ft)
Wing span (swept): 24 m (79 ft)
Wing angle (extended): 70 deg
Wing angle (swept): 30 deg Length 38 m (125 ft)
Height: 10 m (33 ft)
Armament: maximum of 20,000 kg (44,000 lb) of free fall nuclear and conventional bombs, guided munitions, up to 8 cruise missiles, including Kh-101, Kh-55MS (AS-15 Kent) , Kh-15P (AS-16 Kickback)

Unit Cost: $1bn

LAS-AH1 'Harpy'

Following lengthy negotiations with the Kamov design bureau and the Russian Federal government, Lasatanian Aeronautical Industries is delighted to introduce the 'LAS-AH Harpy' attack helicopter to its range. The LAI version features improved engine capability.


The LAS-AH1 Harpy is a state-of-the-art and powerful battle helicopter which is in limited service with the Lasatanian Air Force. This aircraft is not fielded. Only a dozen prototypes exist, and it has not yet been approved for full-scale production. There are two versions of the Harpy. The LAS-AH1 LAS-AH1 'Harpy' is a single seat close support helicopter and the LAS-AH1X 'Hellfire' two seat trainer and combat version.


The coaxial, contrarotating, three-blade main rotors are widely separated with swept-back tips, and there is no tail rotor. The equally tapered, short, stubby, weapon-carrying wings with end plates are mounted on the streamlined fuselage, which tapers to the front and rear. The fuselage, which is flat-bottomed except for the underbelly gun pod and sensor, features a flat plated glassed-in canopy. The tail is thick with a tapering tail boom and back-tapered tail fin with a square tip. The tail flats are high-mounted on the tail boom with end plates, and located forward of the fin. Twin turboshaft engines are mounted high on the fuselage above the stubby wings, with semicircular air intakes and exhausts that are turned outward.

The helicopter has a number of unique characteristics including single seat to increase combat and flight characteristics and reduce operational costs. It was designed for remote operations, and not to need ground maintenance facilities for 2 weeks. The airframe is 35% composite materials with a structural central 1m 2 keel beam of kevlar/ nomex that protects critical systems and ammunition. The fully armored pilot's cabin can withstand 23-mm gunfire, and the cockpit glass 12.7-mm MG gunfire. The Zvezda K-37-800 pilot ejection system functions at any altitude, and enables a successful ejection at low altitude and maximum speed.

External stores are mounted on underwing external hardpoints. Each wing has two hardpoints for a total of four stations. A typical mix for targeting armor formations is 12x AT-16 ATGMs, 500x 30-mm cannon rounds, and 2x 20-round pods of 80-mm folding fin unguided rockets. The 30-mm cannon is the same as on the BMP-2. It also carries guided air-to-air missiles IGLA-V (Needle C), already extensively tested and sold to buyers abroad. The LAS-AH1's avionics is largely in line with what is the norm for one-seater fighters and ground attack jets. It's most remarkable feature is a remote targeting system with a capability to provide for a sudden deadly attack from a distance that rules out direct visual contact with the target. The firing computer will turn the aircraft to keep the gun on target. It is equipped with downlink to provide information from the battlefield. The targeting and control system and weaponry enable accurate target engagement at ranges of up to 10km.


The LAS-AH1 'Harpy' features unique maneuvrability and operating characteristics due to the contra-rotating co-axial rotors. The coaxial counter-rotating rotor system negates the need for a tail rotor and its drive system. Because of this, this aircraft is unaffected by wind strength and direction, has an unlimited hovering turn rate, and gives a smaller profile and acoustic signature, while allowing a 10-15% greater power margin. The HOKUM is fully aerobatic. It can perform loops, roll, and “the funnel”, where the aircraft will maintain a concentrated point of fire while flying circles of varying altitude, elevation, and airspeed around the target.



http://www.fas.org/man/dod-101/sys/ac/row/4001.gif

Specifications

Country of Origin: Russia/Lasatania

Builder: LAI

Role: Antihelicopter and gunship

Blades Main rotor: 6 (2 heads, 3 blades each)

Tail rotor: None

Rotor diameter 14.5 meters

Wing span 7.34 meters

Length rotors turning: 16 meters

fuselage: 15.0 meters

Height gear extended: 4.93 meters

gear retracted: 4 meters

Cargo Compartment Dimensions Negligible

Engines 2x 3,000-shp LAI XRT-27VK turboshaft

Weight Maximum Gross: 10,800 kg

Normal Takeoff: 9,800 kg

Empty: 7,692 kg

Standard Payload External weapons load: 2,500 kg on 4 under-wing stores points.

Speed Maximum (level): 380 km/h

Cruise: 270-310 km/h

Sideward: 100+ km/h, Rearward: 100+ km/h

Turn Rate unlimited

Max “G” Force +3 to +3.5 g

Ceiling Service: 5,500 meters

Hover (out of ground effect): 4,000 meters

Hover (in ground effect): 5,500 meters

Vertical Climb Rate 10 m/s

Fuel (liters) Internal: INA

External Fuel Tank: 500 ea. (max 4x)

Range (km) Maximum Load: INA

Normal Load: 460

With Aux Fuel: INA

Armament

1x 2A42 30-mm cannon [250 HE-Frag + 250 AP]

2 - AT-16 VIKhR ATGM (6 each)

2 - 80-mm rockets (20 each)

2 - Twin 23-mm gun pods [940 rounds]

4 - 500-kg bombs

2 - AA-11/ARCHER AAM

External fuel tanks (500 liters)

30-mm Automatic Cannon, 2A42:

Range: effective 3,000 m

Elevation: -45° to +10°

Traverse: ±15°

Ammo type and rate of fire is selectable by pilot (HE or AP, 350 or 600)

Most Probable Armament:

Fuselage-mounted 30-mm cannon on right side

80-mm rockets

AT-16 VIKhR ATGMs [ATGM racks can depress to 12°]

AVIONICS

The LAS-AH1 'Harpy' uses a low-light level TV or thermal sighting, a laser range-finder (10 km), FLIR, air data sensor, and digital data-link which interface with a fire control com-puter, an autopilot, a helmet sighting system and HUD for target location, acquisition, designation, and firing.

Night/Weather Capabilities:

This aircraft’s avionics package ensuring a full day/night, all weather capability. If it is to be employed at night in an attack role, it must be fitted with a night targeting pod. This pod includes a FLIR, a millimeter wave radar, and an electro-optical sight takes up one of the underwing pylons. The Ka-50N, and Ka-52 are capable of performing attack missions in day/night, and all-weather conditions.


Survivability/Countermeasures

Main rotors and engines electrically deiced.

Infrared signature suppressors can be mounted on engine exhausts.

Radar warning receivers, IFF, chaff and flares.

Armored cockpit and self-sealing fuel tanks.

Pilot ejection system.

Crew 1

Cost: $30M




http://www.fas.org/man/dod-101/sys/ac/row/ka-50-40p06.jpg

http://www.fas.org/man/dod-101/sys/ac/row/ka-50-40p04.jpg

IMPORTANT: TO MAKE AN ORDER GO TO THIS THREAD:

http://forums2.jolt.co.uk/showthread.php?p=6749687#post6749687


(It's just to keep this thread clear for later additions and save space)

I was wondering If I could get some help with my pricing on my Russian Planes. I would like to know of some sites that'll offer me what I need or if you could just let me know what I should price them heres the link (http://forums2.jolt.co.uk/showthread.php?t=341258&page=1&pp=15)

OOC: It's a bit hard to find details on it to be honest, I worked my prices out after hearing that an export MiG-29 will cost $35m, based on that you can kind of work out prices from there... I did come across one site with prices but all it had was the aforementioned MiG-29.. I tend to work it out by finding the price of a comparable western fighter on the net then reducing it by 10% of so, or if its more modern as is the case with the LAS-XF2 and LAS-XF3, I tend to ramp it up a fair bit, given these are premium products... hope this helps!