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PL-17

Chinese long range air-to-air missile From Wikipedia, the free encyclopedia

The PL-17 (NATO reporting name: CH-AA-12 Auger[2]) or PL-20 is an active radar-guided very-long-range air-to-air missile developed by the People's Republic of China for the People's Liberation Army Air Force (PLAAF).[3] The missile has a claimed range of around 400 km (250 mi) and is intended to target high value airborne assets (HVAA) such as tanker and early warning and control (AEW&C) aircraft.[4][5][6]

Quick facts Type, Place of origin ...
PL-17
J-16 armed with PL-17
TypeBeyond-visual-range air-to-air missile (very-long-range)
Place of originPeople's Republic of China
Service history
In service2024–present
Used byPeople's Liberation Army Air Force
People's Liberation Army Naval Air Force
Production history
ManufacturerShanghai Academy of Spaceflight Technology
Specifications

EngineDual-pulsed solid-propellant rocket[1]
Operational
range
~400 km
Guidance
system
Active radar homing/infrared homing /passive radiation homing.[1]
Launch
platform
Close

History and development

The missile was first identified on a Shenyang J-16 fighter in 2016,[7] it was fired in November,[8] and can also be deployed on Chinese imported Su-30MKK and Su-35 fighters.[9] It is understood that PL-17 is a separate development from the ramjet-powered PL-21 (PL-XX).[5][10] PL-17 may have entered PLAAF service in 2024.[11]

Design

PL-17 is much larger than other long-range air-to-air missiles, at 6 m (20 ft) long (whereas PL-15, AIM-120 are measured around 4 m (13 ft) long), which contains more solid fuel. The extended length makes the missile unfit for the internal weapons bay of the Chengdu J-20. During the flight, PL-17 would rely on inertial guidance and satellite navigation to track targets. During the terminal phase, the missile would turn on its multimodal seeker with both active radar and passive sensors.[4] The sensors include, reportedly, a miniature active electronically scanned array (AESA) radar for tracking, passive anti-radiation seeker for locating radar-equipped targets, and a possible optical window feautring an additional infrared seeker as supplement.[12]

The missile body features a low-drag profile, and maneuverability is provided by four small control fins and thrust-vectoring engines.[13] Estimates for its maximum operational range may vary, but the widely reported figure is ~400 km.[14][3] The missile is powered by a dual pulse rocket motor and flies in lofted launch trajectory[4] to achieve the reported range of 400 km (250 mi) class, according to the Royal United Services Institute.[13] It has a top speed in excess of Mach 4.[10][15]

See also

References

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