China Scrambles To Upgrade PL-15 Series of Missiles After India Decodes It
India’s successful recovery of several Chinese-origin PL-15E
beyond-visual-range air-to-air missiles during Operation Sindoor has provided
the nation with an unforeseen technological windfall,
reported Republic World News.
The missiles, reportedly deployed by Pakistan during combat, failed to reach
their targets and landed almost intact in Rajasthan, offering the Defence
Research and Development Organisation (DRDO) and the Indian Air Force a rare
chance to dissect cutting-edge Chinese missile technology.
The PL-15E is known for its dual-pulse rocket motor, active radar seeker, and
advanced data-link—features that previously gave China and its allies a marked
advantage in long-range aerial engagements.
By examining these systems closely, Indian scientists have been able to better
understand Chinese approaches to seeker fidelity, electronic warfare
resilience, and radar signal encoding techniques. These insights are now being
leveraged to refine India’s own ASTRA missile family.
China, meanwhile, has reportedly been unsettled by India’s analytical
progress. Sources within defence intelligence circles suggest that Beijing has
hastened the development of the PL-16 missile—a stealth-optimised derivative
intended to complement the J-20 and future sixth-generation fighters.
The PL-16 is expected to feature improved radar-absorbing materials, a compact
seeker head compatible with conformal weapon bays, and enhanced mid-course
guidance to reduce detection probability during cruise.
For India, the PL-15E analysis has already borne fruit. The ASTRA MK-2,
nearing completion of its trials, builds on several counter-countermeasure
techniques inferred from the Chinese missile’s design, allowing it to resist
electronic jamming and degrade enemy radar locks. The forthcoming ASTRA MK-3,
with an extended range of over 300 kilometres, will utilise a dual-pulse
propulsion system inspired partly by the recovered missile’s efficient burn
pattern.
The incident also underscores a growing contest in electronic warfare and
missile technology across Asia. India’s newfound understanding of China’s
radar-guided missile architecture has allowed it to fine-tune its own signal
processing algorithms, improve home-grown active radar seekers, and enhance
missile data-link encryption.
In parallel, China’s efforts to shield its designs from further compromise are
accelerating through modular architecture updates and encryption algorithm
revisions.
Strategically, the episode marks one of the most consequential intelligence
gains for India in recent decades, narrowing the missile technology gap with
its principal regional rival. With DRDO integrating lessons from the PL-15E
into multiple ongoing projects, including air-to-air and surface-based
interceptors, India’s air combat capability is poised for a substantial leap,
while China races to stay a step ahead.
Comparison Between Chinese PL-15 And India's ASTRA Missiles
| Specification | PL-15 (China) | PL-15E (Pakistan) | PL-16 (China) | Astra MK-2 (India) | Astra MK-3 (India) |
|---|---|---|---|---|---|
| Type | Long-range active radar-guided AAM | Export variant of PL-15 | Stealthier, compact version of PL-15 | Indigenous long-range air-to-air missile | Advanced version of Astra MK-2 |
| Length | ~4 meters | ~4 meters | Smaller than PL-15 (~compressed airframe) | Comparable to legacy Astra (~3.8m approx.) | Similar or slightly larger than MK-2 |
| Diameter | ~200 mm | ~200 mm | Smaller diameter (compressed design) | Approx. 180-200 mm | Approx. 180-200 mm |
| Range | 200–300 km | 145 km | Similar or better than PL-15 range | ~150 km | Over 300 km |
| Speed | Mach 5+ | Mach 5+ | Mach 5+ | Around Mach 4+ | Above Mach 5 |
| Propulsion | Dual-pulse solid rocket motor | Dual-pulse solid rocket motor | High-performance dual-pulse rocket motor | Dual-pulse solid rocket motor | Enhanced dual-pulse propulsion |
| Warhead | 20–25 kg fragmentation | 20–25 kg fragmentation | Similar or improved warhead | Approx. 15-20 kg fragmentation | Approx. 20 kg fragmentation |
| Guidance & Nav | Inertial, Beidou satellite, two-way datalink, AESA radar seeker | Same as PL-15 with possible reduced ECM capability | AESA radar seeker, two-way datalink with enhanced ECCM | Active radar seeker with improved ECCM | Active radar seeker with further improved ECCM |
| Launch Platforms | Chinese fighters including J-20, J-10C, J-16 | Pakistan's JF-17 Block III, J-10CE | Designed for internal bays of J-20 and possibly J-35 | Indian Air Force fighters (Tejas, Su-30 dependent on integration) | Expected for future indigenous fighters and upgrades |
| Stealth Compatibility | Limited (PL-15 with cropped fins) | Folding fins for stealth compatibility | Designed for stealth fighters with smaller size and folded fins | No full stealth compatibility | Improved stealth compatibility |
| Special Features | Dual-pulse motor for range and terminal speed, GaN AESA seeker for high ECM resistance | Compact for export, maintains key tech features | Smaller size allows more missiles in stealth bays | ECM lessons incorporated from PL-15 teardown | Incorporates range/speed and ECCM improvements from PL-15 tech insights |
Based On Republic World Video Report
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