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Python 3
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Launch of Python 3 missile from F-4.
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Python 3 is a third generation short to medium range air-to-air missile adapted to the F-15, F-16, all types of Mirage, F-5, F-4 and Kfir C-2 and C-7 aircraft.
The Python 3 was rushed into service during the Lebanon War in 1982 , with pre-production rounds being tested in actual air-to-air combat against Syrian aircraft. The conventional rod-type high-explosive warhead weighs 11 kg . It has a maximum range of about 15 kilometers and a maximum speed of Mach 3.5. The infrared seeker of the Python 3 has a plus or minus 30-degree gimbal angle and can be operated in boresight, uncaged, or radar-slaved mode. The Python 3 is claimed by Israel to have a speed, turning radius, and range superior to that of the AIM-9L Sidewinder.
The missile upgrades the capability of its carrier and gives it air superiority in modern air combat scenarios, such as:
Head-on interceptions
Beam interceptions
Dogfights involving high-g maneuvers
Low-altitude interceptions of helicopters and light aircraft
Self-defense air combat during penetration missions.
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Main Featurs
All-aspect capability, including head-on interception
Effective against most evasive tactics
Capable of intercepting low-signature and low-altitude threats
15 km maximum effective range at high altitude
Active proximity fuze, based on lead bias navigation system
Highly efficient warhead
Versatile target acquisition modes, including slaving to advanced radar system
Reliability greater than 95%
Full ILS, including combat doctrine manual, training and ground support equipment |
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The Python 3, air-to-air missile, has intercepted dozens of Syrian planes. In Lebanon War (1982) more than 50 enemy planes were destroyed with Python 3 missiles. The pilot can launch the missile only after steering his plane at the enemy plane at a 30 degree cone. |
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PL-8 |
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The PL-8 infrared homing short-range air-to-air missile is a Chinese licensed production version of the Israeli Python 3. China and Israel agreed on the deal of Python 3 technology and its licensed production in 1982, and the transfer began in September 1983. The first batch of the PL-8 rolled out between March 1988 and April 1989.
To streamline the design, development, manufacture, and marketing of the air-to-air missile, in the mid-1980s China integrated most of its air-to-air missile R&D teams and manufacturing facilities located in different regions into one AAM complex, known as Luoyang Electro-Optics Technology Development Centre (EOTDC) . The PL-8 became the first project undertaken by this centre. In 2002 the centre was rename as China Academy of Air-to-Air Missile after Shaanxi Hanzhong Air-to-Air Missile Factory (also known as Hanzhong Nanfeng Machine Factory) was relocated to Luoyang and merged with the centre.
As China's first all-aspect infrared homing short-range air-to-air missile, the PL-8 is currently in service with the PLA Air Force and Naval Aviation Troops in a significant number. The later versions of PL-8 were reported to have been integrated with helmet-mounted sight (HMS) to improve the performance.
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Length |
295 cm |
Span |
80 cm |
Body |
15 cm |
Weight |
120 kg (warhead 11kg) |
Guidance Type |
IR |
Model |
1 x spr. |
Range |
15 km |
Speed |
3.5 Mach |
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