Tuesday, January 12, 2010

jf 17 thunder pakistan




Chengdu JF-17 Xiaolong/Thunder
Origin: China/Pakistan
Type: Multi-role attack aircraft
Max Speed: Mach 1.6
Max Range: 648 nm/1,200 km
Dimensions: span 29 ft 6 in/9.0 m, length 45 ft 11 in/ 14.0 m, height 16 ft 8 in/5.1 m
Weight: empty weight 13,904 lb/6,320 kg, max take-off weight 27,940 lb/12,700 kg
Powerplant: single klimov RD-93 turbofan
Armament: 1x23mm GSh-23-2 cannon pod on centerline, max weapon load 8,380 lb/3,800 kg
Operators: China ((FC-1)), Pakistan ((JF-17))

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Saturday, January 9, 2010

Chengdu J-10


Chengdu J-10
Origin: China
Type: multi-purpose fighter
Max Speed: Mach 1.85
Max Range: 1,149 miles/1,850 km
Dimensions: span 11.3 m/37.2 ft, length 16.5 m/54.0 ft, height 6.0 m/19.7 ft
Weight: empty weight 15,299 lbs/6,940 kg max take-off weight 40,564 lb/18,400 kg
Powerplant: one Saturn/Lyulka AL-31FN turbofan engine with 19,334lbs static thrust with afterburner and 27,562 lbs without afterburner, alternatively with a Chinese WPS-12 turbofan engine.
Armament: A combination of short range air-air PL-8 missiles, medium range air-air PL-11 missiles and additional tanks, air to ground rockets, bombs and a minimum of seven to a maximum of eleven weapon stations. Maximum weapon load around 18,518 lbs/8,400 kg. Built-in 23mm or 30mm cannon.
Operators: China, Pakistan

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Wednesday, January 6, 2010

Chengdu F-7/J-7 Airguard


Chengdu F-7/J-7 Airguard
Origin: China

Type: Fighter
Max Speed: 1,175 kt / 1,350 mph
Max Range: 600 km / 373 miles
Dimensions: span 7.154 m / 23 ft 5.625 in length 13.945 m / 45 ft 9 in height 4.103 m / 13 ft 5.5 in
Weight: empty 5275 kg / 11,629 lb normal take-off 7531 kg / 16,603 lb
Powerplant: one Liyang (LMC) Wopen WP-7B(BM) rated at 43.15 kN (9.700 Ib st) dry and 59.82 kN (13,448 Ib st) with afterburning. This is derived from the TumanskiiR-1 IF-300
Armament: Two internal 30 mm Type 30-1 cannon or One 23 mm Type 23-3 cannon AIM-9L Sidewinder; PL-2, PL-5, bombs; rockets
Operators: Albania (J-7I), Bangladesh (J-7II), China (J-7I), China (J-7II), China (J-7III), Egypt (F-7), Egypt (J-7II), Iran (J-7II), Myanmar (J-7II), Pakistan (F-7), Pakistan (J-7II), Sri Lanka, Sudan (J-7II), Tanzania (J-7I), Zimbabwe (J-7II)

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Nanchang Q-5 Fantan


Nanchang Q-5 Fantan
Origin: China
Type: close-support fighter with secondary air combat capability
Max Speed: 642 kt / 739 mph
Max Range: 2,000 km / 1,243 miles
Dimensions: span 9.68 m / 31 ft 9 in length 15.65 m / 51 ft 4.25 in height 4.33 m / 14 ft 2.75 in
Weight: empty 6,375 kg / 14,054 lb max. take-off 11,830 kg / 26,080 lb
Powerplant: two 3250-kg (7,165-lb) afterburning thrust Shenyang WP-6 (Tumanskii R-9BF811) turbojets
Armament: two 23-mm Type 23-2K cannon with 100 rounds per gun; provision for 2000 kg (4,409 Ib) of disposable stores, including AAMs, free-fall bombs, cluster bombs, rocket-launcher pods, napalm tanks, drop tanks and ECMS pods, on 10 external hardpoints
Operators: Bangladesh, China, Myanmar, North Korea, Pakistan, Sudan

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Lockheed Martin F-16C/D Fighting Falcon



Lockheed Martin F-16C/D Fighting Falcon
Origin: USA
Type: single-seat air-combat and multi-role fighter
Max Speed: 1,146 kt / 1,320 mph
Max Range: 3,886 km / 2,415 miles
Dimensions: span 10.00 m / 32 ft 9.75 in length 15.03 m / 49 ft 4 in height 5.09 m / 16 ft 8.5 in
Weight: empty 8,273 kg / 18,218 lb max. take-off 19,187 lb
Powerplant: one 13154-kg (29,000-lb) afterburning thrust Pratt & Whitney F100-PW-229 or General Electric F110-GE-129 turbofan
Armament: one 20-mm M61A1 Vulcan cannon with 500 rounds, plus provision for up to 9276 kg (20,450 Ib) of externa ordnance on one underfuselage, six underwing and two tip hardpoints, this total declining to 5420 kg (11,950 Ib) for sorties including 9-g manoeuvres; the ordnance can include AIM-9 Sidewinder and AIM-120 AMRAAM air-to-air missiles, a wide range of disposable ordnance (free-tall and guided), drop tanks and electronic pods (ECM, reconnaissance and targeting)
Operators: Bahrain, Chile, Egypt, Greece, Israel, Morocco (Ordered), Oman, Pakistan (Ordered), Poland, Singapore, South Korea, Turkey, United Arab Emirates, United States
Aircraft Overview:

The F-16 Fighting Falcon is the first operational fighter to employ fly-by-wire flight controls, relaxed static stability, high-g cockpit, bubble canopy, variable camber wings, blended wing-body design, modular construction, and integrated digital avionics.

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Lockheed Martin F-16A/B Fighting Falcon



Lockheed Martin F-16A/B Fighting Falcon
Origin: USA
Type: single-seat air-combat and multi-role fighter
Max Speed: 1,146 kt / 1,320 mph
Max Range: 3,886 km / 2,415 miles
Dimensions: span 10.00 m / 32 ft 9.75 in length 15.03 m / 49 ft 4 in height 5.09 m / 16 ft 8.5 in
Weight: empty 8,273 kg / 18,218 lb max. take-off 19,187 lb
Powerplant: one 13154-kg (29,000-lb) afterburning thrust Pratt & Whitney F100-PW-229 or General Electric F110-GE-129 turbofan
Armament: one 20-mm M61A1 Vulcan cannon with 500 rounds, plus provision for up to 9276 kg (20,450 Ib) of externa ordnance on one underfuselage, six underwing and two tip hardpoints, this total declining to 5420 kg (11,950 Ib) for sorties including 9-g manoeuvres; the ordnance can include AIM-9 Sidewinder and AIM-120 AMRAAM air-to-air missiles, a wide range of disposable ordnance (free-tall and guided), drop tanks and electronic pods (ECM, reconnaissance and targeting)
Operators: Belgium, Denmark, Egypt, Indonesia, Israel, Italy, Jordan, Netherlands, Norway, Pakistan, Portugal, Taiwan, Thailand, United States, Venezuela

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