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Kh-31 KRYPTON / AS-17


-Picture of Kh-31P-

-Picture of Kh-31-
Comparison with other Missiles

New air defense weapon systems of the American Patriot kind have raised the requirements which anti-radar missiles must meet. These include first of all higher speed and longer range, then also high interference immunity and radar turn-off when attacked.

For the special purpose of meeting these requirements, the "Zvezda" group under the direction of V. Bugayskiy began in 1977 working on the Kh-31 missile (Article) 77P). The first launching of this missile took place in 1982.

The most interesting component of the Kh-31P is its dual propulsion system designed by the "Soyuz" Design Bureau in Turayevo near Moscow (note: there are several "Soyuz" engineering groups in Russia). First the missile is accelerated by its solid-fuel rocket engine to a speed of Mach 1.8, then the engine is discarded and the interior of the missile is converted into the combustion chamber of the missile's jet engine.The latter accelerates the missile to a speed of almost Mach 4.5, while four air intake holes on the sides of the missile body open up. On the basis of the Kh-31P anti radar missile were developed the Kh-31A missile (Article 77A) with an active-radar guidance head and also an M-31 flying target for air defense training exercises.


Sources:
Global Security

Accreditation:
cipher for the Kh-31 image
RaptorR3d for the Comparison image

*Original Article by "Millie"*