fighter

Fighter planes are one thing which make me excited. So I just pull out few of my favorite fighter planes and put up here. They are fast and deadly!

F-16 Fighting Falcon
A USAF F-16C over Iraq in 2008
Role	Multirole jet fighter
National origin	United States
Manufacturer	General Dynamics Lockheed Martin
First flight	2 February 1974
Introduction	17 August 1978
Status	Active, in production
Primary users	United States Air Force 25 other users (see operators page)
Number built	4,450+
Unit cost	F-16A/B: US$14.6 million (1998 dollars)[1] F-16C/D: US$18.8 million (1998 dollars)[1]
Variants	General Dynamics F-16 VISTA
Developed into	Vought Model 1600 General Dynamics F-16XL General characteristics Crew: 1 Length: 49 ft 5 in (15.06 m) Wingspan: 32 ft 8 in (9.96 m) Height: 16 ft (4.88 m) Wing area: 300 ft² (27.87 m²) Airfoil: NACA 64A204 root and tip Empty weight: 18,900 lb (8,570 kg) Loaded weight: 26,500 lb (12,000 kg) Max takeoff weight: 42,300 lb (19,200 kg) Powerplant: 1 × F110-GE-100 afterburning turbofan Dry thrust: 17,155 lbf (76.3 kN) Thrust with afterburner: 28,600 lbf (127 kN) Performance Maximum speed: At sea level: Mach 1.2 (915 mph, 1,470 km/h)[44] At altitude: Mach 2+ (1,500 mph, 2,410 km/h[1]) clean configuration Combat radius: 340 mi (295 nmi, 550 km) on a hi-lo-hi mission with six 1,000 lb (450 kg) bombs Ferry range: 2,280 NM (2,620 mi, 4,220 km) with drop tanks Service ceiling: 60,000+ ft (18,000+ m) Rate of climb: 50,000 ft/min (254 m/s) Wing loading: 88.3 lb/ft² (431 kg/m²) Thrust/weight: 1.095 Armament Guns: 1× 20 mm (0.787 in) M61 Vulcan 6-barreled gatling cannon, 511 rounds Hardpoints: 2× wing-tip Air-to-air missile launch rails, 6× under-wing & 3× under-fuselage pylon stations holding up to 17,000 lb (7,700 kg) of payload Rockets: 4× LAU-61/LAU-68 rocket pods (each with 19× /7× Hydra 70 mm rockets, respectively) or 4× LAU-5003 rocket pods (each with 19× CRV7 70 mm rockets) or 4× LAU-10 rocket pods (each with 4× Zuni 127 mm rockets) Missiles: Air-to-air missiles: 2× AIM-7 Sparrow or 6× AIM-9 Sidewinder or 6× IRIS-T or 6× AIM-120 AMRAAM or 6× Python-4 Air-to-ground missiles: 6× AGM-45 Shrike or 6× AGM-65 Maverick or 4× AGM-88 HARM Anti-ship missiles: 2× AGM-84 Harpoon or 4× AGM-119 Penguin Bombs: 8× CBU-87 Combined Effects Munition 8× CBU-89 Gator mine 8× CBU-97 Sensor Fuzed Weapon Wind Corrected Munitions Dispenser capable 4× GBU-10 Paveway II 6× GBU-12 Paveway II 4× JDAM 4× Mark 84 general-purpose bombs 8× Mark 83 GP bombs 12× Mark 82 GP bombs 8× Small Diameter Bomb 3× B61 nuclear bomb Others: SUU-42A/A Flares/Infrared decoys dispenser pod and chaff pod or AN/ALQ-131 & AN/ALQ-184 ECM pods or LANTIRN, Lockheed Martin Sniper XR & LITENING targeting pods or up to 3× 300/330/370 US gallon Sargent Fletcher drop tanks for ferry flight/extended range/loitering time. Avionics AN/APG-68 radar [edit] Notable appearances in media Main article: F-16 Fighting Falcon in fiction Mitsubishi F-2

F/A-18 Hornet
A U.S. Marine Corps F/A-18C
Role	Multirole fighter
National origin	United States
Manufacturer	McDonnell Douglas / Boeing Northrop
First flight	18 November 1978
Introduction	7 January 1983
Status	In service
Primary users	United States Navy United States Marine Corps Royal Australian Air Force Spanish Air Force
Number built	F/A-18A/B/C/D: 1,480[1]
Unit cost	US$29–57 million (2006)[2]
Developed from	Northrop YF-17
Variants	McDonnell Douglas CF-18 Hornet High Alpha Research Vehicle
Developed intoGeneral characteristics Crew: F/A-18C: 1, F/A-18D: 2 (pilot and weapons system officer) Length: 56 ft (17.1 m) Wingspan: 40 ft (12.3 m) Height: 15 ft 4 in (4.7 m) Wing area: 400 ft² (38 m²) Airfoil: NACA 65A005 mod root, 65A003.5 mod tip Empty weight: 23,000 lb (10,400 kg) Loaded weight: 36,970 lb (16,770 kg) Max takeoff weight: 51,900 lb (23,500 kg) Powerplant: 2 × General Electric F404-GE-402 turbofans Dry thrust: 11,000 lbf (48.9 kN) each Thrust with afterburner: 17,750 lbf (79.2 kN) each Performance Maximum speed: Mach 1.8 (1,190 mph, 1,915 km/h) at 40,000 ft (12,190 m) Range: 1,089 nmi (1,250 miles, 2,000 km) with only two AIM-9s Combat radius: 400 nmi (460 mi, 740 km) on air-air mission Ferry range: 1,800 nmi (2,070 mi, 3,330 km) Service ceiling: 50,000 ft (15,240 m) Rate of climb: 50,000 ft/min (254 m/s) Wing loading: 93 lb/ft² (454 kg/m²) Thrust/weight: 0.96 The M61 Vulcan at the Miramar Airshow Using multiple ejector racks: ten AIM-120 AMRAAMs and two AIM-9 Sidewinders Armament Guns: 1× 20 mm (0.787 in) M61 Vulcan nose mounted 6-barreled gatling cannon, 578 rounds Hardpoints: 9 total: 2× wingtips missile launch rail, 4× under-wing, and 3× under-fuselage with a capacity of 13,700 lb (6,215 kg) external fuel and ordnance Rockets: 2.75 inches (70 mm) Hydra 70 rockets 5 in (127.0 mm) Zuni rockets Missiles: Air-to-air missiles: 4× AIM-9 Sidewinder or 4× AIM-132 ASRAAM or 4× IRIS-T or 4× AIM-120 AMRAAM, and 2× AIM-7 Sparrow or additional 2× AIM-120 AMRAAM Air-to-surface missiles: AGM-65 Maverick Standoff Land Attack Missile (SLAM-ER) AGM-88 HARM Anti-radiation missile (ARM) AGM-154 Joint Standoff Weapon (JSOW) Taurus missile (Cruise missile) Anti-ship missile: AGM-84 Harpoon Bombs: JDAM Precision-guided munition (PGMs) Paveway series of Laser guided bombs Mk 80 series of unguided iron bombs CBU-87 cluster CBU-89 gator mine CBU-97 Mk 20 Rockeye II B61/Mk57 nuclear bombs[86] Others: SUU-42A/A Flares/Infrared decoys dispenser pod and chaff pod or Electronic countermeasures (ECM) pod or AN/AAS-38 Nite Hawk Targeting pods (US Navy only), to be replaced by AN/ASQ-228 ATFLIR or LITENING targeting pod (USMC, Royal Australian Air Force, Spanish Air Force, and Finnish Air Force only) or up to 3× 330 US gallons (1,200 l; 270 imp gal) Sargent Fletcher drop tanks for ferry flight or extended range/loitering time. Avionics Hughes APG-73 radar ROVER (Remotely Operated Video Enhanced Receiver) antenna for use by US Navy's F/A-18C strike fighter squadrons Inertial navigation system GPS Two mission computers HUD cockpit dislay Very High Frequency omni-directional landing system Multiple-functioning Cathode ray tube display	Boeing F/A-18E/F Super Hornet Boeing X-53 Active Aeroelastic Wing

F-35 Lightning II
An F-35C Lightning II, marked CF-1, conducts a test flight over the Chesapeake Bay
Role	Stealth multirole fighter
National origin	United States
Manufacturer	Lockheed Martin Aeronautics
First flight	15 December 2006
Introduction	2016[1]–2018[2][3]
Status	In initial production, in U.S. service as a training aircraft[4]
Produced	2006–present
Number built	13 flight-test aircraft[N 1]
Unit cost	F-35A: US$122 million (flyaway cost, 2011)[7] F-35B: US$150M (avg. cost, 2011)[8] F-35C: US$139.5M (avg. cost, 2011)[8][9] Note: Average costs excludes development cost[8] F-35A weapons system unit cost is US$183.5M (FY 2011)[7]
Developed from	Lockheed Martin X-35

General characteristics

• Crew: 1
• Length: 51.4 ft (15.67 m)
• Wingspan: 35 ft^{[N 6]} (10.7 m)
• Height: 14.2 ft^{[N 7]} (4.33 m)
• Wing area: 460 ft²^[113] (42.7 m²)
• Empty weight: 29,300 lb (13,300 kg)
• Loaded weight: 49,540 lb^{[75][N 8][283]} (22,470 kg)
• Max takeoff weight: 70,000 lb^{[N 9]} (31,800 kg)
• Powerplant: 1 × Pratt & Whitney F135 afterburning turbofan
  • Dry thrust: 28,000 lbf^{[284][N 10]} (125 kN)
  • Thrust with afterburner: 43,000 lbf^[284][285] (191 kN)
• Internal fuel capacity: 18,480 lb (8,382 kg)^{[N 11]}

Performance

• Maximum speed: Mach 1.6+^[108] (1,200 mph, 1,930 km/h) Tested to Mach 1.53.^[286]
• Range: 1,200 nmi (2,220 km) on internal fuel
• Combat radius: over 590 nmi^{[N 12]} (1,090 km) on internal fuel^[287]
• Service ceiling: 60,000 ft^[288] (18,288 m)
• Rate of climb: classified (not publicly available)
• Wing loading: 91.4 lb/ft² (446 kg/m²)
• Thrust/weight: **With full fuel: 0.87
  • With 50% fuel: 1.07
• g-Limits: 9 g^{[N 13]}

Armament

• Guns: 1 × General Dynamics GAU-22/A Equalizer 25 mm (0.984 in) 4-barreled gatling cannon, internally mounted with 180 rounds^{[N 14][108]}
• Hardpoints: 6 × external pylons on wings with a capacity of 15,000 lb (6,800 kg)^[108][113] and 2 internal bays with 2 pylons each^[113] for a total weapons payload of 18,000 lb (8,100 kg)^[76] and provisions to carry combinations of:
  • Missiles: ** Air-to-air missiles:
    • AIM-120 AMRAAM
    • AIM-132 ASRAAM
    • AIM-9X Sidewinder
    • IRIS-T
    • MBDA Meteor (Pending further funding)^[289]
    • JDRADM (after 2020)^[290]
  • Air-to-surface missiles:
    • AGM-154 JSOW
    • AGM-158 JASSM^[114]
    • Brimstone missile
    • Joint Air-to-Ground Missile
    • SOM
  • Anti-ship missiles:
    • JSM
  • Bombs: ***Mark 84, Mark 83 and Mark 82 GP bombs
    • Mk.20 Rockeye II cluster bomb
    • Wind Corrected Munitions Dispenser capable
    • Paveway-series laser-guided bombs
    • Small Diameter Bomb (SDB)
    • JDAM-series
    • B61 nuclear bomb^[291]

Avionics

• Northrop Grumman Electronic Systems AN/APG-81 AESA radar
• Northrop Grumman Electronic Systems AN/AAQ-37 Distributed Aperture System (DAS) missile warning system
• BAE Systems AN/ASQ-239 (Barracuda) electronic warfare system
• Harris Corporation Multifunction Advanced Data Link (MADL) communication system

Differences between variants

	F-35A CTOL	F-35B STOVL	F-35C Carrier version
Length	51.4 ft (15.7 m)	51.3 ft (15.6 m)	51.5 ft (15.7 m)
Wingspan	35 ft (10.7 m)	35 ft (10.7 m)	43 ft (13.1 m)
Wing Area	460 ft² (42.7 m²)	460 ft² (42.7 m²)	668 ft² (62.1 m²)
Empty weight	29,300 lb (13,300 kg)	32,000 lb (14,500 kg)	34,800 lb (15,800 kg)
Internal fuel	18,500 lb (8,390 kg)	13,300 lb (6,030 kg)	19,600 lb (8,890 kg)
Max takeoff weight	70,000 lb (31,800 kg)	60,000 lb (27,000 kg)	70,000 lb (31,800 kg)
Range	1,200 nmi (2,220 km)	900 nmi (1,670 km)	1,400 nmi (2,520 km)
Combat radius on internal fuel	590 nmi (1,090 km)	450 nmi (833 km)	640 nmi (1,185 km)
Thrust/weight full fuel 50% fuel	0.87 1.07	0.90 1.04	0.75 0.91

Su-30
Su-30 of the Russian Air Force in flight over Russia
Role	Multirole fighter[1]
Manufacturer	Sukhoi
First flight	31 December 1989
Introduction	1996
Status	Operational
Primary users	Indian Air Force PLA Air Force (China) Venezuelan Air Force See Operators section for others
Unit cost	US$33–45 million
Developed from	Sukhoi Su-27
Variants	Sukhoi Su-30MKI Sukhoi Su-30MKK

General characteristics

• Crew: 2
• Length: 21.935 m (72.97 ft)
• Wingspan: 14.7 m (48.2 ft)
• Height: 6.36 m (20.85 ft)
• Wing area: 62.0 m² (667 ft²)
• Empty weight: 17,700  kg (39,021 lb)
• Loaded weight: 24,900 kg (54,900 lb)
• Max takeoff weight: 34,500 kg (76,060 lb)
• Powerplant: 2 × AL-31FL low-bypass turbofans
  • Dry thrust: 7,600 kgf (74.5 kN, 16,750 lbf) each
  • Thrust with afterburner: 12,500 kgf (122.58 kN, 27,560 lbf) each

Performance

• Maximum speed: Mach 2.0 (2,120 km/h, 1,320 mph)
• Range: 3,000 km (1,620 nmi) at altitude
• Service ceiling: 17,300 m (56,800 ft)
• Rate of climb: 230 m/s (45,275 ft/min)
• Wing loading: 401 kg/m² (82.3 lb/ft²)
• Thrust/weight: 0.98

Armament
The Su-27PU had 8 hardpoints for its weapon load, whereas the Su-30MK's combat load is mounted on 12 hardpoints: 2 wingtip AAM launch rails, 3 pylons under each wing, 1 pylon under each engine nacelle, and 2 pylons in tandem in the "arch" between the engines. All versions can carry up to 8 tonnes of external stores.

• Guns: 1 × GSh-30-1 gun (30 mm calibre, 150 rounds)
• AAMs: 6 × R-27ER1 (AA-10C), 2 × R-27ET1 (AA-10D), 6 × R-73E (AA-11), 6 × R-77 RVV-AE (AA-12)
• ASMs: 6 × Kh-31P/Kh-31A anti-radar missiles, 6 × Kh-29T/L laser guided missiles, 2 × Kh-59ME
• Aerial bombs: 6 × KAB 500KR, 3 × KAB-1500KR, 8 × FAB-500T, 28 × OFAB-250-270, nuclear bombs

[edit] Incidents and accidents

• 12 June 1999: Paris Air Show, Le Bourget, France, a Russian Su-30MK crashed — both pilots ejected safely and no one was hurt on the ground. (Video)
• 30 April 2009: an Indian Air Force Su-30MKI crashed near Jaisalmer. A pilot died.^[38]
• 30 November 2009: an Indian Air Force Su-30MKI crashed near Jaisalmer. The pilots survived.^[39]

[edit] See also

Aviation portal

• Fourth generation jet fighter

Related development

• Sukhoi Su-27
• Sukhoi Su-33
• Sukhoi Su-34
• Sukhoi Su-35
• Sukhoi Su-37
• Shenyang J-11

F-22 Raptor
The F-22 Raptor
Role	Stealth air superiority fighter
National origin	United States
Manufacturer	Lockheed Martin Aeronautics Boeing Defense, Space & Security
First flight	7 September 1997[1]
Introduction	15 December 2005
Status	In service
Primary user	United States Air Force
Number built	173 as of September 2011 (187 planned)[2]
Program cost	US$66.7 billion[3]
Unit cost	US$150 million (flyaway cost for FY2009)[4]
Developed from	Lockheed YF-22
Developed into	Lockheed Martin X-44 MANTA Lockheed Martin FB-22

General characteristics

• Crew: 1
• Length: 62 ft 1 in (18.90 m)
• Wingspan: 44 ft 6 in (13.56 m)
• Height: 16 ft 8 in (5.08 m)
• Wing area: 840 ft² (78.04 m²)
• Airfoil: NACA 64A?05.92 root, NACA 64A?04.29 tip
• Empty weight: 43,430 lb (19,700 kg^[6][233])
• Loaded weight: 64,460 lb (29,300 kg^{[N 6]})
• Max takeoff weight: 83,500 lb (38,000 kg)
• Powerplant: 2 × Pratt & Whitney F119-PW-100 Pitch Thrust vectoring turbofans
  • Dry thrust: 23,500 lb^[235] (104 kN) each
  • Thrust with afterburner: 35,000+ lb^[6][235] (156+ kN) each
• Fuel capacity: 18,000 lb (8,200 kg) internally,^[6][233] or 26,000 lb (11,900 kg) with two external fuel tanks^[6][233]

Performance

• Maximum speed: **At altitude: Mach 2.25 (1,500 mph, 2,410 km/h)^[115]
  • Supercruise: Mach 1.82 (1,220 mph, 1,963 km/h)^[115]
• Range: >1,600 nmi (1,840 mi, 2,960 km) with 2 external fuel tanks
• Combat radius: 410 nmi^[232] (471 mi, 759 km)
• Ferry range: 2,000 mi (1,738 nmi, 3,219 km)
• Service ceiling: 65,000 ft (19,812 m)
• Wing loading: 77 lb/ft² (375 kg/m²)
• Thrust/weight: 1.08 (1.26 with loaded weight & 50% fuel)
• Maximum design g-load: -3.0/+9.0 g^[115]

USAF poster overview of key features and armament

Armament

• Guns: 1× 20 mm (0.787 in) M61A2 Vulcan 6-barreled gatling cannon in starboard wing root, 480 rounds
• Air to air loadout:
  • 6× AIM-120 AMRAAM
  • 2× AIM-9 Sidewinder
• Air to ground loadout:
  • 2× AIM-120 AMRAAM and
  • 2× AIM-9 Sidewinder for self-protection, and one of the following:
    • 2× 1,000 lb (450 kg) JDAM or
    • 8× 250 lb (110 kg) GBU-39 Small Diameter Bombs
• Hardpoints: 4× under-wing pylon stations can be fitted to carry 600 US gallon drop tanks or weapons, each with a capacity of 5,000 lb (2,268 kg).^[236]

Avionics

• RWR (Radar warning receiver): 250 nmi (463 km) or more^[125]
• Radar: 125–150 miles (200–240 km) against 1 m² (11 sq ft) targets (estimated range)^[123]
• Chemring MJU-39/40 flares for protection against IR missiles.^[237]

This fighter made by chengdu aircraft china republik. the specification like f-16 early varion blok 10-15 but the price is more low because not to longer to finish the riset. 19million US$ (19.000.000)

MIG-29 fighter plane.
THE KNIGHT RUSSIAN FIGHTER rival FIGHTING FALCON. 29million US$ (29.000.000)

Sukhoi-30 fighter plane. Multi role function can be ground fighter or bomber and dog fight in space.
40 million US$(40.000.000).

Sukhoi-27 fighter plane.
Flanker family, can be used from  CARRIER VESSEL (cv) .
30 millionUS$ (30.000.000).

A-4 SkyHawk Firing.MARINES VERSION, 20Million US$ (25.000.000). The standard version more low. only afew nation still operated this fihter.

F-15  Strike Eagle (All variation)-US$57.8 million (57.800.000).  F-15  Eagle                               -US$31.1 million (31.100.000)  The main power of NAVY SEAL to be superior in the sky and sea.  Its the legendary TOM CAT twin engine and larger multi role fighter. only us navy seal use it. US$38 million (38.000.000).     F-5 tiger the most succesfull fighter in the 80's more 60 country use it. US$ 2.1 million( 2.100.000). its all upgrade variant.   F-4 Phantom (all variants)- $2.4 (2.400.000) US.  The Legendary ground attack in iraq freedom with jump jet harrier. F-111 Aardvark (All Variants)-$10.3 million (10.300.000). Its the bomber variant.   F-117  Night hawk (All variants)-$111,2 (111.000.200) Data dari National Museum[9] Karakteristik umum Kru: 1 Panjang: 65 ft 11 in Lebar sayap: 43 ft 4 in Tinggi: 12 ft 9.5 in Luas sayap: 780 ft² Bobot kosong: 29,500 lb Bobot terisi: 52,500 lb Mesin: 2× General Electric F404-F1D2 turbofans, 10,600 lbf masing-masing Kinerja Laju maksimum: Mach 0.92 (617 mph, 993 km/h) Laju jelajah: Mach 0.92 Jarak jangkau: 930 NM[10] Batas tertinggi servis: 69,000 ft Beban sayap: 65 lb/ft² Dorongan/berat: 0.40 Persenjataan 2 × internal weapons bays with one hardpoint each (total of two weapons) equipped to carry: Bombs: BLU-109 hardened penetrator GBU-10 Paveway II laser-guided bomb GBU-12 Paveway II laser-guided bomb GBU-27 Paveway III laser-guided bomb JDAM INS/GPS guided munition GBU-10 GBU-12 GBU-27 GBU-31 Persenjataan F117 F-2 A Mitsubishi F-2A Role Multirole fighter National origin Japan, United States Manufacturer Mitsubishi Heavy Industries, Lockheed Martin First flight 7 October 1995 Introduction 2000 Primary user Japan Air Self-Defense Force Number built 94, plus 4 prototypes[1] Unit cost ¥12 billion yen; $127 million (constant 2009 USD)[2] Developed from F-16 Block 40 JAS 39 Gripen Swedish Air Force JAS 39 Gripen Role Multirole fighter Manufacturer Saab AB First flight 9 December 1988 Introduction 1 November 1997 Status Active service Primary users Swedish Air Force South African Air Force Czech Air Force Hungarian Air Force Unit cost US$ 40–60 million[1][2]
Tornado IDS/ECR Tornado IDS Luftwaffe Jerman  Tipe Serang darat Perang Elektronika  Produsen Panavia Aircraft GmbH  Terbang perdana 14 Agustus 1974  Diperkenalkan 1979  Status Operasional  Pengguna Royal Air Force Bundeswehr - (Luftwaffe dan Marine) Italia Arab Saudi  Tahun produksi 1979-1999  Jumlah produksi 992  Varian Panavia Tornado ADV
Karakteristik umum Kru: 2 Panjang: 16.72 m Lebar sayap: 13.91 m at 25° wing sweep, 8.60 m at 67° wing sweep Tinggi: 5.95 m Luas sayap: 26.6 m² Bobot kosong: 13,890 kg Bobot maksimum lepas landas: 28,000 kg Mesin: 2× Turbo-Union RB199-34R Mk 103 afterburning turbofans Dorongan kering: 43.8 kN masing-masing Dorongan dengan pembakar lanjut: 76.8 kN masing-masing Kinerja Laju maksimum: 800kts IAS Mach 2.34 (2,417.6 km/h, 1,511 mph) Jarak jangkau: 1,390 km typical combat Jarak jangkau ferri: 3,890 km with four external drop tanks Batas tertinggi servis: 15,240 m Laju panjat: 76.7 m/s Dorongan/berat: 0.55 Persenjataan Senjata api: 2× 27 mm Mauser BK-27 cannon with 180 rounds per gun (versus 1× BK-27 mounted on Panavia Tornado ADV) Titik keras: 4× light duty + 3× heavy duty under-fuselage and 4× swivelling under-wing pylon stations holding up to 9000 kg (19,800 lb) of payload, the two inner wing pylons have shoulder launch rails for 2× Short-Range AAM (SRAAM) each Roket: None Rudal: Air-to-air missiles: AIM-9 Sidewinder or IRIS-T or AIM-132 ASRAAM for self-defence Air-to-surface missiles: 6× AGM-65 Maverick; or 12× Brimstone missile (12 being the maximum operational limit carried by RAF's Tornado GR4); or 4× Storm Shadow or Taurus KEPD 350 cruise missile Anti-ship missiles: 2× AS.34 Kormoran; or 2× BAe Sea Eagle; or Anti-radiation missiles: 4× AGM-88 HARM; or 9× ALARM missile Bom: Hunting Engineering BL755 cluster bombs; or HOPE/HOSBO GPS/electro-optically guided glide bombs; or Joint Direct Attack Munition; or Paveway series of Laser-guided bomb (LGB); or Up to 2× JP233 or MW-1 munitions dispensers (for runway cratering operations) Up to 4× B61 or WE.177 tactical nuclear weapons Others: Up to 4× drop tanks for ferry flight/extended range/loitering time Avionik RAPTOR aerial reconnaissance pod RAFAEL LITENING targeting pod; or TIALD laser designator pod PRICE (GR4 or F3)-$27Million(21.000.000) Mirage 2000N/D Mirage 2000N at the Radom Air Show, Poland Role Fighter-bomber Manufacturer Dassault Aviation First flight 3 February 1986 Number built 75[citation needed] Developed from Mirage 2000 General characteristics Crew: 2 Length: 14.55 m (47 ft 9 in) Wingspan: 9.13 m (29 ft 11 in) Height: 5.15 m (16 ft 11 in) Wing area: 41 m² (440 ft²) Empty weight: 7,600 kg (17,000 lb) Loaded weight: 10,680 kg (23,550 lb) Max takeoff weight: 17,000 kg (38,000 lb) Powerplant: 1 × SNECMA M53-P2 afterburning turbofan Dry thrust: 64 kN (14,300 lbf) Thrust with afterburner: 95.1 kN (21,400 lbf) Performance Maximum speed: 2,338 km/h (1,289 kn, 1,453 mph) Combat radius: 800 NM (1,480 km, 920 mi) Ferry range: 1,800 NM (3,340 km, 2,100 mi) Service ceiling: 18,000 m (59,000 ft) Rate of climb: 285 m/s (56,000 ft/min) Wing loading: 410 kg/m² (85 lb/ft²) Thrust/weight: 0.91 Armament Hardpoints: 4× under-wing 4× under fusolage 1× centerline Rockets: Up to 4x Matra SNEB 68-mm 18-round rocket pods on the four underwing hardpoints Missiles: Air-to-air missiles: Up to 4× R550 Magic air-to-air missiles for self-defence, normally 2 on the ouboard underwing pylons Up to 4× MICA IR air to air missiles for self-defence, normally 2 on the ouboard underwing pylons Air-to-ground missiles: - Mirage 2000N 1× ASMP medium-range nuclear missile on the centerline pylon Air-to-ground missiles: - Mirage 2000D 1× Apache anti-runway cruise missile on the centerline pylon 1× SCALP EG air launched cruise missile on the centerline pylon 2× AS-30L laser guided missiles on the inboard underwing pylons Bombs: AASM 125, 250, 1000 Kg laser, ISN/GPS, IIR guided bombs. The lighter versions are carried in pairs on the centerline and inboard wing hardpoints and one under each of the four fuselage hardpoints up to 10× GBU-12 227 Kg laser guided bombs, in pairs on the centerline and inboard wing hardpoints and one under each of the four fuselage hardpoints up to 3× GBU-16 454 Kg laser guided bombs on the centerline and inboard wing hardpoints up to 3× GBU-10 907 Kg laser guided bombs on the centerline and inboard wing hardpoints up to 3× GBU-24 907 Kg laser guided bombs on the centerline and inboard wing hardpoints up to 3× BGL-400 400 Kg laser guided bombs on the centerline and inboard wing hardpoints up to 3× BGL-1000 1000 Kg laser guided bombs on the centerline and inboard wing hardpoints Avionics Twin inertial navigation system Antilope 5 terrain-following radar [edit] See also Wikimedia Commons has media related to: Dassault Mirage 2000 Related development Dassault Mirage 2000 Dassault Mirage 4000 Mirage 2000D/N-$23 Million (23.000.000) Mirage F1 A Mirage F1B Role Fighter aircraft Manufacturer Dassault Aviation First flight 23 December 1966 Introduction 1973 Primary users French Air Force Iran Air Force Spanish Air Force Royal Moroccan Air Force Number built >720 Developed from Dassault Mirage III Mirage F1 - $11 Million (11,000,000) Rafale A Rafale B (foreground), and a Rafale C (background) of the French Air Force Role Multirole fighter aircraft National origin France Manufacturer Dassault Aviation First flight 4 July 1986 Introduction 4 December 2000 Status In production, in service Primary users French Air Force French Navy Program cost €39.6 billion (1 January 2008[1]) Unit cost Rafale C: €64 million, US$82.3 million (flyaway cost, 2008)[1] Rafale M: €70 million, US$90.5 million (flyaway cost, 2008)[1] Unit cost: €163 million US$227.8 million 2010)[2] Su-34 Su-34 taking off Role Fighter-bomber[1] Manufacturer Sukhoi First flight 13 April 1990 Introduction 21 December 2009[2] Status In production[3] Primary user Russian Air Force Produced 2006–present[4] Number built 28 Unit cost US$36 million[5] Developed from Sukhoi Su-27 Specifications (Su-34) Data from Sukhoi data,[27] Gordon and Davison[28] AF Technology,[29] Airwar.ru[30] General characteristics Crew: 2 Length: 23.34 m (72 ft 2 in) Wingspan: 14.7 m (48 ft 3 in) Height: 6.09 m (19 ft 5 in) Loaded weight: 39,000 kg (85,980 lb) Useful load: 8,000 kg (17,600 lb) Max takeoff weight: 45,100 kg (99,425 lb) Powerplant: 2 × Lyulka AL-31FM1[31] turbofans, 13,500 kgf (132 kN, 29,762 lbf) with afterburner each Performance Maximum speed: High altitude: Mach 1.8 (1,900 km/h, 1,180 mph) Low altitude: Mach 1.2 (1,400 km/h, 870 mph) at sea level Combat radius: 1,100 km (680 mi) Ferry range: 4,000 km (2,490 mi) Service ceiling: 15,000 m (49,200 ft) Wing loading: 629 kg/m² (129 lb/ft²) Thrust/weight: 0.68 Armament Guns: 1 × 30 mm GSh-30-1 (9A-4071K) cannon, 180 rounds Hardpoints: 12 × wing and fuselage stations with a capacity of 8,000 kg (17,630 lb) and provisions to carry combinations of: Missiles: R-27 air-to-air missile R-73 air-to-air missile R-77 air-to-air missile Kh-29L/T (AS-14) Kh-25MT/ML/MP (AS-10) Kh-59 (AS-18) Kh-58 (AS-11) Kh-31P (AS-17) Kh-35 Ural (AS-20) Kh-65S OR Kh-SD Moskit or P-800 Oniks anti-ship missile Bombs: KAB-500L OR KAB-500KR KAB-1500L/KR guided bombs FAB-250,FAB-500,FAB-1500 unguided bombs S-8, S-13, S-25 rocket pods Other: fuel tanks, EW and reconnaissance pods, nuclear bombs. [edit] See also Aviation portal Related development Sukhoi Su-30 Sukhoi Su-33 Sukhoi Su-35 AV-8B Harrier II A United States Marine Corps AV-8B hovering Role V/STOL ground-attack aircraft National origin United States / United Kingdom Manufacturer McDonnell Douglas / British Aerospace Boeing / BAE Systems First flight YAV-8B: 9 November 1978[1] AV-8B: 5 November 1981[2] Introduction August 1985[3] Status Out of production, in service Primary users United States Marine Corps Spanish Navy Italian Navy Produced 1981–2003[4] Program cost US$6.5 billion (1987)[5] Unit cost US$24–30 million[6] Developed from Hawker Siddeley Harrier Variants British Aerospace Harrier II Specifications (AV-8B Harrier II Plus) External images Armament and vectored nozzles Underside of AV-8 Harrier II Data from Nordeen,[116] Boeing[117] General characteristics Crew: 1 pilot Length: 46 ft 4 in (14.12 m) Wingspan: 30 ft 4 in (9.25 m) Height: 11 ft 8 in (3.55 m) Wing area: 243.4 ft² (22.61 m²) Airfoil: supercritical airfoil Empty weight: 13,968 lb (6,340 kg) Loaded weight: 22,950 lb (10,410 kg) Max takeoff weight: Rolling: 31,000 lb (14,100 kg) Vertical: 20,755 lb (9,415 kg) Powerplant: 1 × Rolls-Royce F402-RR-408 (Mk 107) vectored-thrust turbofan, 23,500 lbf (105 kN) Performance Maximum speed: Mach 1.0 (585 knots, 673 mph, 1,083 km/h) Range: 1,200 nmi (1,400 mi, 2,200 km) Combat radius: 300 nmi (350 mi, 556 km) Ferry range: 1,800 nmi (2,100 mi, 3,300 km) Rate of climb: 14,700 ft/min (4,485 m/min) Wing loading: 94.29 lb/ft² (460.4 kg/m²) Armament Guns: 1× General Dynamics GAU-12 Equalizer 25 mm (0.984 in) 5-barreled gatling cannon mounted under-fuselage in the left pod, with 300 rounds of ammunition in the right pod Hardpoints: 6× under-wing pylon stations holding up to 13,200 lb (5,988 kg) of payload: Rockets: 4× LAU-5003 rocket pods (each with 19× CRV7 70 mm rockets) Missiles: Air-to-air missiles: 4× AIM-9 Sidewinder or similar-sized infrared-guided missiles 6× AIM-120 AMRAAM (on radar equipped AV-8B Plus variants) Air-to-surface missiles: 6× AGM-65 Maverick; or 2× AGM-84 Harpoon; or 2× AGM-88 HARM Bombs: CBU-100 cluster bombs (CBUs) Mark 80 series of unguided bombs (including 3 kg and 14 kg practice bombs) Paveway series of laser-guided bombs (LGBs) Mark 77 napalm canisters Others: up to 4× 300/330/370 US Gallon drop tanks (pylon stations No. 2, 3, 4 & 5 are wet plumbed) Avionics Raytheon APG-65 radar AN/AAQ-28V LITENING targeting pod (on radar-equipped AV-8B Plus variants) Special note: An upgrade program is currently fitting airframes with wiring and software to employ 1760 bus-based smart weapons, such as Joint Direct Attack Munitions Eurofighter Typhoon A Eurofighter Typhoon of the Austrian Air Force Role Multirole fighter Manufacturer Eurofighter GmbH First flight 27 March 1994[1] Introduction 4 August 2003 Status Operational Primary users Royal Air Force Luftwaffe Italian Air Force Spanish Air Force See Operators section for others Number built >260 as of January 2011[2] 471 ordered (as of January 2009) Unit cost €90 million (system cost Tranche 3A)[3] £125m (including development + production costs)[4] Developed from British Aerospace EAP Variants Eurofighter Typhoon variants General characteristics Crew: 1 (operational aircraft) or 2 (training aircraft) Length: 15.96 m (52.4 ft) Wingspan: 10.95 m (35.9 ft) Height: 5.28 m (17.3 ft) Wing area: 51.2 m2[221] (551 sq ft) Empty weight: 11,150 kg (24,600 lb) Loaded weight: 16,000 kg[221][222] (35,000 lb) Max takeoff weight: 23,500 kg (52,000 lb) Powerplant: 2 × Eurojet EJ200 afterburning turbofan Dry thrust: 60 kN (13,000 lbf) each Thrust with afterburner: 89 kN (20,000 lbf) each Fuel capacity: 4,500 kg (9,900 lb) internal[221] Performance Maximum speed: **At altitude: Mach 2 (2,495 km/h/1,550 mph)[223][224][225] At sea level: Mach 1.2[220] (1,470 km/h/910 mph)[226] Supercruise: Mach 1.1–1.5[227] Range: 2,900 km (1,800 mi) Combat radius: Ground attack, lo-lo-lo: 601 km (325 nmi) Ground attack, hi-lo-hi: 1,389 km (750 nmi) Air defence with 3-hr combat air patrol: 185 km (100 nmi) Air defence with 10-min. loiter: 1,389 km (750 nmi) [221][228] Ferry range: 3,790 km (2,350 mi) Service ceiling: 19,810 m[229] (64,990 ft) Rate of climb: >315 m/s[230][231] (62,000 ft/min[232]) Wing loading: 312 kg/m2[221] (64.0 lb/ft2) Thrust/weight: 1.15 g-limits: +9/−3 g[233] Armament Guns: 1 × 27 mm Mauser BK-27 Revolver cannon with 150 rounds Hardpoints: Total of 13: 8 × under-wing; and 5 × under-fuselage pylon stations; holding up to 7,500 kg (16,500 lb) of payload[221][234] Missiles: Air-to-air missiles: AIM-9 Sidewinder AIM-132 ASRAAM AIM-120 AMRAAM IRIS-T MBDA Meteor, in the future Air-to-surface missiles: AGM-65 Maverick, in the future AGM-88 HARM, in the future Storm Shadow (AKA Scalp EG), in the future Brimstone, in the future Taurus KEPD 350 Penguin, in the future AGM Armiger, in the future Bombs: 6× 500lb Paveway™ IV Paveway II/III/Enhanced Paveway series of laser-guided bombs (LGBs) Joint Direct Attack Munition (JDAM), in the future HOPE/HOSBO, in the future Others: Flares/infrared decoys dispenser pod chaff pods Electronic countermeasures (ECM) pods LITENING III laser targeting pod Up to 3 drop tanks for ferry flight or extended range/loitering time. Avionics Euroradar CAPTOR Radar Passive Infra-Red Airborne Tracking Equipment (PIRATE) [edit] See also Aviation portal Eurofighter Typhoon timeline Related development British Aerospace EAP Related lists List of active United Kingdom military aircraft List of aircraft of the Royal Air Force List of military aircraft of Germany List of megaprojects, Aerospace Jaguar A French Air Force Jaguar A during a refuelling mission over the Adriatic Sea, in support of Operation Joint Forge Role Ground attack Manufacturer SEPECAT (Breguet/BAC) First flight 8 September 1968 Introduction 1973 Retired 2005 (France) / 2007 (UK) Status Active Primary users Royal Air Force (historical) French Air Force (historical) Indian Air Force Royal Air Force of Oman Number built 543[1] Unit cost US$8 million in 1978[2] General characteristics Crew: One Length: 16.83 m (55 ft 2½ in) Wingspan: 8.69 m (28 ft 6 in) Height: 4.89 m (16 ft 0½ in) Wing area: 24.2 m² (220 ft²) Aspect ratio: 3.12:1 Empty weight: 7,000 kg (15,432 lb) Loaded weight: 10,954 kg (24,149 lb) Max takeoff weight: 15,700 kg (34,612 lb) Powerplant: 2 × Rolls-Royce/Turbomeca Adour Mk 102 turbofans Dry thrust: 22.75 kN (5,115 lbf) each Thrust with afterburner: 32.5 kN (7,305 lbf) each Performance Maximum speed: Mach 1.6 (1,699 km/h, 917 knots, 1,056 mph) at 11,000 m (36,000 ft) Combat radius: 908 km (490 nmi, 564 mi) (lo-lo-lo, external fuel) Ferry range: 3,524 km (1,902 nmi, 2,190 mi) Service ceiling: 14,000 m[136] (45,900 ft) Climb to 9,145 m (30,000 ft): 1 min 30 sec[136] Armament Guns: 2× 30 mm (1.18 in) DEFA cannons, 150 rounds/gun Hardpoints: 5 total: 4× under-wing and 1× center-line pylon stations with a capacity of 10,000 lb (4,500 kg) and provisions to carry combinations of: Rockets: 8× Matra rocket pods with 18× SNEB 68 mm rockets each Missiles: AS.37 Martel anti-radar missiles or AS-30L laser guided air-to-ground missile. 2× R550 Magic air-to-air missiles on underwing pylons Bombs: various unguided or laser-guided bombs or 1× AN-52 nuclear bomb Other: ECM protection pods, Reconnaissance Pod, ATLIS laser/electro-optical targeting pod, external drop tanks for extended range/loitering time [edit] See also Royal Air Force portal Aviation portal Comparable aircraft LTV A-7 Corsair II IAR-93 Mikoyan MiG-27 Mitsubishi F-1 Soko J-22 Orao Xian JH-7 If i am missing Aircraft ,or you want to add more aircraft , or just want to leave a comment please post it under this forum and i will respond as soon as possible or send a E-mail toNEOBAR.JKL12@GMAIL.COM WEAPON AND AIR FRAME NOT INCLUDED.