F-2

Specifications

Maximum Weight: 22000 kg
Power of Engine: 13200kg
Maximum Speed: 2300 km/h
Maximum Altitude: 20000 m
Radius of Action: 1000 km
Weapons: 1gun (20mm)

Missiles:
• AAM-1
• AAM-3
• Maverik
• ASM-2
• bombs

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F-1

Specifications

Type: F-1
Function: attack
Year: 1977
Crew: 1
Engines: 2 * 3300kg Ishikawajima-Harime TF40-801A
Wing Span: 7.88m
Length: 17.66m
Height: 4.39m
Wing Area: 21.18m2
Empty Weight: 6358kg
Max.Weight: 13674kg
Speed: 1700km/h
Ceiling: 15250m
Range: 1130km
Internal Fuel: 3054 kg
Drop Tanks: 833 L drop tank with 659kg of fuel for 126nm range
In-Flight Refueling: No
Payload: 2722kg
Sensors: J/AWG-12 radar, RWR, basic bombsite
Armament:
• Cannon: 1 20mm Vulcan
• Type 80 ASM
• Mk82 500lb bombs
• M117 750lb bombs
• LAU-69 rocket pods
• AAM-1
• AIM-9L

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HF-24 Marut

Specifications
Year: 1961
Crew: 1
Engines: 2 * 2200kg HAL/R.R. Orpheus Mk.703
Wing Span: 9.00m
Length: 15.87m
Height: 3.60m
Wing Area: 28m2
Empty Weight: 6195kg
Max. Weight: 10908kg
Speed: 1128km/h
Ceiling: 13750m
Range: 800km
Armament: 4*g30mm 48*r68mm 1814kg
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Hindustan (HAL) Tejas / Light Combat Aircraft (LCA) Light Multi-Role Fighter

HISTORY:
First Flight: (TD-1) 4 January 2001
Service Entry: planned for 2010

CREW: one: pilot

ESTIMATED COST: $21 million

AIRFOIL SECTIONS:
Wing Root: unknown
Wing Tip: unknown

DIMENSIONS:
Length: 43.27 ft (13.20 m)
Wingspan: 26.88 ft (8.20 m)
Height: 14.42 ft (4.40 m)
Wing Area: 412.6 ft² (38.4 m²)
Canard Area: not applicable

WEIGHTS:
Empty: 12,125 lb (5,500 kg)
Normal Takeoff: 18,740 lb (8,500 kg) [clean]
Max Takeoff: 27,560 lb (12,500 kg)
Fuel Capacity: internal: 795 gal (3,000 L); external: 1,055 gal (4,000 L)
Max Payload: 8,820 lb (4,000 kg)

PROPULSION:
Powerplant: (prototypes) one General Electric F404-F2J3 or F404-IN20 turbofan; (production) one GTRE GTX-35VS Kaveri turbofan
Thrust: (F404-F2J3) 18,100 lb (80.50 kN); (F404-IN20) 18,700 lb (83.18 kN); (GTX) 20,200 lb (89.86 kN)

PERFORMANCE:
Max Level Speed: at altitude: 1,195 mph (1,920 km/h) at 36,000 ft (11,000 m), Mach 1.8; at sea level: unknown
Initial Climb Rate: unknown
Service Ceiling: 50,000 ft (15,250 m)
Range: 460 nm (850 km)
g-Limits: +9 / -3.5

ARMAMENT:
Gun: one 23-mm GSh-23 twin-barrel cannon (220 rds)
Stations: eight external hardpoints
Air-to-Air Missile: R-77/AA-12 Adder, R-73/AA-11 Archer, BVRAAM
Air-to-Surface Missile: up to two conventional cruise missiles, anti-ship missiles
Bomb: laser-guided bombs, conventional bombs, cluster bombs
Other: rocket pods

KNOWN VARIANTS:
LCA-TD-1: First technology demonstrator equipped with a General Electric F404-F2J3 turbofan
LCA-TD-2: Second technology demonstrator
LCA-PV-1 and PV-2: Single-seat prototype vehicles
LCA-PV-3: Single-seat prototype vehicle that should be at or very close to production form, equipped with in-flight refueling capability
LCA-PV-4: Single-seat prototype vehicle for a naval variant
LCA-PV-5: Two-seat trainer prototype vehicle
Tejas: Production model for the Indian Air Force
Trainer: Two-seat trainer model
Navy model: A navalized version with strengthened landing gear and a redesigned forward fuselage to be used aboard a future Indian aircraft carrier
MCA: Planned Medium Combat Aircraft derived from the LCA, supposed to possess greater stealth characteristics and thrust-vectoring capability

KNOWN COMBAT RECORD: not yet in service

KNOWN OPERATORS:
India, Bharatiya Vayu Sena (Indian Air Force)
India (Indian Naval Air Squadron) Selengkapnya...

Chengdu J-10, F-10 Multi-Role Fighter

HISTORY:
First Flight: 24 March 1998
Service Entry: 2004 or 2005

CREW: 1 pilot

DIMENSIONS:
Length :47.86 ft (14.57 m)
Wingspan/Lebar Sayap: 28.75 ft (8.78 m)
Height: 15.75 ft (4.80 m)
Wing Area: 355.2 ft2 (33 m2)
Canard Area: 58.55 ft2 (5.45 m2)

WEIGHTS:
Empty : 15,300 lb (6,940 kg)
Typical Load: unknown
Max Takeoff : 40,565 lb (18,400 kg)
Fuel Capacity: internal: unknown, external: unknown
Max Payload: 18,520 lb (8,400 kg)

PROPULSION:
Powerplant : one Saturn/Lyulka AL-31F afterburning turbofan
Thrust: 27,560 lb (122.6 kN)

PERFORMANCE:
Max Level Speed: at altitude: Mach 1.85; at sea level: unknown
Initial Climb Rate : unknown
Tinggi Max: unknown
Jarak Tempuh: 1,000 nm (1,850 km)
g-Limits: unknown

ARMAMENT:
Gun: probably one 23-mm or 30-mm cannon
Stations : eleven external hardpoints and two wingtip rails
Air-to-Air Missile : PL-8, PL-10
Air-to-Surface Missile: unknown
Bomb: unknown

KNOWN VARIANTS:
J-10: Prototype fighter

KNOWN OPERATORS: China


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T-90

Type: Main battle tank
Place of origin: Russia
Service history: Used by Russia and India
Status: Operational

Production history
Designer: Kartsev-Venediktov
Designed: 1993
Manufacturer: Uralvagonzavod
Unit cost: 35,226,000 RUB; $1,371,000 USD
Produced: 1995 - Present


Specifications

Weight: 46.5 tonnes
Length: 9.53 m (31.27 ft)
Width: 3.78 m (9.12 ft)
Height: 2.22 m (7.28 ft)
Crew: 3
Suspension: torsion bar

Armor: Classified steel-composite-reactive blend
Primary armament: 125 mm smoothbore gun with ATGM capability; mainly 9M119 Svir
Secondary armament: 7.62 mm coaxial machine gun, 12.7 mm anti-aircraft machine gun

Engine: Model 84 V-84 12-cyl. diesel; V-92 12-cyl. diesel; V-96 12-cyl. diesel
Power: 840 hp (626 kW) for Model 84 V-84 12-cyl. diesel engine; 950 hp (708 kW) for V-92 12-cyl. diesel engine; 1,100 hp (820 kW) for V-96 12-cyl. diesel engine
Power/weight: 18.1 hp/tonne (13.5 kW/tonne) for Model 84 V-84 12-cyl. diesel engine; 20.4 hp/tonne (15.2 kW/tonne) for V-92 12-cyl. diesel engine; 23.7 hp/tonne (17.6 kW/tonne) for V-96 12-cyl. diesel engine
Range: 650 km
Speed: 65 km/h

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T-72

Specifications: T-72

Length: 22.80ft (6.95m)
Width: 11.78ft (3.59m)
Height: 7.28ft (2.22m)

Performance:
Speed: 42mph (67km/h)
Range: 300miles (483km)

Crew: 3
Weight: 50.7 US Short Tons (46,000kg)

Systems:
NBC Protection: Yes
Nightvision: Yes - Infrared

Power:
Engine(s): 1 x V-84 V-12 Piston air-cooled multi-fuel diesel engine generating 840hp @ 2,000rpm.

Armament & Ammunition:
1 x 125mm main gun
1 x 12.7mm machine gun
1 x 7.62mm coaxial machine gun
2 x 6 smoke grenade dischargers
Ammunition:
45 x 125mm projectiles
300 x 12.7mm ammunition
2,000 x 7.62mm ammunition
12 x smoke grenades

Variants:
T-72 - Base production model
T-72K - Commander's Base-version Vehicle
T-72A - Various modifications
T-72AK - Commander's A-version Vehicle
T-72AV - Features explosive reactive armor
T-72M - Export model of T72A
T-72M1 - Additional armor; Modernized variant
T-72B - Additional turret armor
T-72BK - Commander's B-version Vehicle
T-72B1 - Sans anti-tank launcher
T-72S - Export variant of T72B model
T-72S1 - Export variant of T72B1 model
T-72BM - Features updated explosive reactive armor.
T-90
P-T91 - Polish-produced T72
TR-125 - Romamian-produced T72
M-84 Degmen - Croatian-produced T72
T-72 155mm - Trialed
T-72 120mm - Trialed
MTU-72 AVLB - Bridgelayer
BREM-1 - Armored Recovery Vehicle
IMR-2 - Battlefield Engineering Vehicle
BMR-3M - Anti-mine Vehicle
BMPT - Armor Support Vehicle
T-72M4 CZ

Designation: T-72
Classification Type: Main Battle Tank
Contractor: Chelybinsk, Nizhnyi Tagil and Kirov - Russia
Country of Origin: Soviet Union
Initial Year of Service: 1974
Number Built: Not Available

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