RIM-116 Rolling Airframe Missile (RAM)

Karakteristik Umum (Block 1)

Fungsi Primer: Surface-to-Air Missile
Kontraktor: Raytheon, Diehl BGT Defence
Panjang: 2780 mm
Diameterr: 127 mm
Fin span: 445 mm
Kecepatan: Mach 2.0+
Warhead: 11.3 kg blast fragmentation
Launch Weight: 73.5 kg (162 lb)
Jarak tempuh: 7.5 km
Sistem Navigasi: three modes—passive radio frequency/infrared homing, infrared only, or infrared dual mode enabled (radio frequency and infrared homing)
Harga: $444,000
Date Deployed: 1992




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USS Nimitz

Ordered: 31 Maret 1967
Mulai Pembuatan: 22 Juni 1968
Peluncuran: 13 Mei 1972
Peresmian: 3 Mei 1975
Kelas: CVN-68
Homeport: NB San Diego, California
Motto: Teamwork, a Tradition
Julukan: "Old Salt"
Pembuat: Newport News Shipbuilding Co., Newport News, Va.

Displacement: Sekitar 97,000 ton (87,996.9 metric tons) full load
Panjang: Keseluruhan: 1,092 ft (333 m), Waterline: 1,040 ft (317 m)
Lebar: Keseluruhan: 252 ft (76.8 m), Waterline: 134 ft (40.8 m)
Draft*: Maximum navigational: 37 ft (11.3 m), Limit: 41 ft (12.5 m)
Propulsion: 2 × Westinghouse A4W nuclear reactors, 4 × steam turbines, 4 × shafts, 260,000 shp (194 MW)
Speed:30+ knots (56+ km/h)
Jarak Tempuh: Tak Terbatas
Complement: Ship's company: 3,200, Air wing: 2,480
Sensors and processing systems: AN/SPS-48E 3-D air search radar, AN/SPS-49(V)5 2-D air search radar, Mk 23 target acquisition radar, 2 × AN/SPN-46 air traffic control radars, AN/SPN-43B air traffic control radar, AN/SPN-44 landing aid radars, 3 × Mk 91 NSSM guidance systems, 3 × Mk 95 radars
Electronic warfare and decoys: SLQ-32A(V)4 Countermeasures suite, SLQ-25A Nixie torpedo countermeasures
Armament: three Rolling Airframe Missile (RAM) launchers, three Mk 29 NATO Sea Sparrow launchers
Armor: Unknown
Jumlah Pesawat: 90 fixed wing and helicopters
Ketapel: 4
Elevator Pesawat: 4


Nimitz Carrier Battle Group
USS Nimitz merupakan bagian dari Carrier Strike Group 11 (CSG-11) dengan Carrier Air Wing 11 di atasnya, dengan Nimitz sebagai pimpinannya dan sebagai tempat komandan Destroyer Squadron 23.

Ships of DESRON-23 (Destroyer Squadron):
- USS Chafee (DDG 90)
- USS Higgins (DDG 76)
- USS John Paul Jones (DDG 53)
- USS Pinckney (DDG 91)
- USS Sampson (DDG 102)

Squadrons of CVW-11:
- Strike Fighter Squadron 14 (VFA-14) "Tophatters"
- Strike Fighter Squadron 41 (VFA-41) "Black Aces"
- Strike Fighter Squadron 81 (VFA-81) "Sunliners"
- Marine Fighter Attack Squadron 232 (VMFA-232) "Red Devils"
- Electronic Attack Squadron 135 (VAQ-135) "Black Ravens"
- Carrier Airborne Early Warning Squadron 117 (VAW-117) "Wallbangers"
- Helicopter Antisubmarine Squadron 6 (HS-6) "Indians"
- Fleet Logistics Support Squadron 30 Detachment 4 (VRC 30) "Providers" Selengkapnya...

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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