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...
Senin, 03 Agustus 2009
Hindustan (HAL) Tejas / Light Combat Aircraft (LCA) Light Multi-Role Fighter
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
Selengkapnya...
T-90
Type: Main battle tankPlace of origin: Russia
Service history: Used by Russia and India
Status: Operational
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
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
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
Merkava Mk 1 / Mk 2 (Chariot)
Classification Type: Main Battle Tank
Contractor: Israeli Ordnance Corps Facility - Israel
Country of Origin: Israel
Initial Year of Service: 1979
Number Built: 1,000
Specifications: Merkava Mk 1 / Mk 2 (Chariot)Dimensions:
Length: 28.31ft (8.63m)
Width: 12.14ft (3.70m)
Height: 9.02ft (2.75m)
Performance:
Speed: 29mph (46km/h)
Range: 249miles (400km)
Structure:
Accommodation: 4
Weight: 66.1 US Short Tons (60,000kg)
Systems:
NBC Protection: Yes
Nightvision: Yes
Power:
Engine(s): 1 x General Dynamics Land Systems AVDS-1790-6A V-12 with an output of 900hp.
Armament & Ammunition:
1 x 105mm main gun
1 x 7.62mm co-axial machine gun
2 x 7.62mm machine guns
1 x 60mm mortar launcher
Ammunition:
62 x 105mm projectiles
10,000 x 7.62mm ammunition
Variants:
Merkava Mk 1 - Initial Production Model Designation.
Merkava Mk 2 - Improved armor protection; improved range; updated fire control system; improved 60mm roof-mounted mortar launcher.
Merkava Mk 3 - 120mm main gun with upgraded powerpack at 1,200hp; new transmission system; improved suspension and fire control system; new threat warning system.
Merkava Mk 3 Baz - Improved armor protection
Merkava Mk 4 - Latest production version.
"Slammer" - Self-Propelled 155mm Gun (prototype)
ARV - Armored Recovery Vehicle (prototype) Selengkapnya...
Duro Dakovic M95 Degman)
Specifications
Designation: Duro Dakovic M95 Degman
Length: 33.27 ft | 10.14 m
Width: 11.78 ft | 3.59 m
Height: 7.19 ft | 2.19 m
Engine(s): 1 x 12-cylinder diesel generating 1,000hp. There is also an optional 1,200hp diesel engine.
Weight: 49.1 tons (US Short) | 44,500 kg
Max Speed: 43 mph | 70 km/h
Max Range: 435 miles | 700 km
Armament: 1 x 125mm main gun; 1 x 7.62mm coaxial machine gun; 1 x 12.7mm anti-aircraft machine gun; 2 x 6 smoke dischargers
Ammunition: 42 x 125mm projectiles; 2,000 x 7.62mm ammunition; 360 x 12.7mm ammunition; 12 x smoke grenades
NBC Protection: Yes
Night Vision: Yes
Crew: 3
Operators: Croatia
Selengkapnya...
Postingan
