HQ-19 Anti-Ballistic Missile Interceptor
The HQ-9B, HQ-19 [THAAD counterpart], HQ-26 [SM-3 counterpart] and HQ-29 [PAC-3 counterpart] are designed primarily for Anti Ballistic Missile capabilities. While the HQ-9A air defense variant of the HQ-9 series is very well attested, the remaining theater missile defense interceptors are poorly attested, and verge on being little more than rumors.(huh?
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It is believed by some that the Russian S-400 Triumf surface-to-air missile system was a joint development program, but others say that HQ-19 has nothing to do with S-400 [according to one source, "and I say this with certainty." China has shown interest in acquiring Russia’s newest long-range SAM, the S-400 TRIUMF, but a contract has not been signed yet and Russian officials have stated China would not receive the S-400 until at least 2017. This SAM can target aircraft, cruise missiles, and tactical and medium-range ballistic missiles.
The only official document that clearly states the designation HQ-19 is a document entitled "The needs analysis propulsion system of tactical missiles and direction of development for solid propellant engine", dating from 2000 and written by the Institute 41 CCAC Group (China Aerospace Science and Technology Corporation). This paper analyzes firstly the risks and types of conflict that China may face up to 2010 (The document is dated 2000, and speaks of "in 10 years"), and gives types of tactical missiles to develop a priority to deal with these external threats. In subsection 3.4, a priority is given to the need for an anti-missile system capable of intercepting high altitude heads ballistic missile whose range is 3000km, phase re-entry. And in response to this paragraph 3.4, in section 4.4 it is clearly stated "Developing solid propellant engines that meet the needs of anti-missile systems area at high altitude," a concept close to American THAAD ( Terminal High Altitude Area Defense).
Finally, in paragraph 5.4 of the document, it gives the status of the development of the HQ-19 motor - a solid propellant engine demonstration with a specific impulse of 260s, mass ratio of 0.85 and able to provide the necessary power for maneuverability 60g to track down the head of ballistic missile, a "completed the design phase, fabrication and testing", "testing validated the carbon fiber shell and propellant N-15B."
The HQ-19 missile is a project launched in the late 1990s. In 1995 the Chinese started serious studies of a kinetic kill vehicle KKV under Program 863. In 1986, to meet the global challenges of new technology revolution and competition, four Chinese scientists, WANG Daheng, WANG Ganchang, YANG Jiachi, and CHEN Fangyun, jointly proposed to accelerate China’s high-tech development. With strategic vision and resolution, the late Chinese leader Mr. DENG Xiaoping personally approved the National High-tech R&D Program, namely the 863 Program. Implemented during three successive Five-year Plans, the program has boosted China’s overall high-tech development, R&D capacity, socio-economic development, and national security. In April 2001, the Chinese State Council approved continued implementation of the program in the 10th Five-year Plan. As one of the national S&T program trilogy in the 10th Five-year Plan, 863 Program continues to play its important role.
In 1999, the first Chinese KKV made the suspension tests successfully flight, China became the second country in the world to have mastered the technology. The first test of V & V was held in 2003 with success. It was in final certification. HQ-19 has a KKV of about 35kg, the system performance would be similar to the US THAAD. Another R & D document mentions a technology demonstration at the HQ-19 engines in 2000, led by the Academy 4 CCAC group. The demonstration also validated "hull carbon fiber" and "rocket N-15B".
HQ-19 Anti-Ballistic Missile Interceptor