Английская Википедия:AIST (missile)

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Версия от 02:04, 27 декабря 2023; EducationBot (обсуждение | вклад) (Новая страница: «{{Английская Википедия/Панель перехода}} {{Infobox weapon |is_missile=yes |name=AIST |image= |origin=Belarus |type=Long-range, all-weather, subsonic cruise missile |used_by=Belarus Army |manufacturer=GVPK (initially) |service=unknown |engine=MS-400 turbofan engine |weight=1500 kg |length=1100 mm |height=455 mm |diameter=0,57 m |wingspan={{convert|8|ft|9|in|m|abbr=on}} |speed=Subsonic; up to 900 km/h }} '''AIST'''...»)
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Шаблон:Infobox weapon AIST cruise missile - latest development of the Belarusian State Military Industrial Committee.[1] The cruise missile is a high precision short-range subsonic cruise missile developed in close cooperation with Ukrainian[2] and Chinese[3] experts.

Overview

The likeliest missile launcher for the cruise missile Aist is supposed to be the universal multiple launch rocket system (MLRS) Polonez,[4] based on a wheeled chassis MZKT-7930 Astrolog.

Vehicles of this type are widely used as a platform for a number of weapon systems, mainly those produced in Russia. Belarusian 4x4 wheeled chassis, in particular, are used as a platform for the Russian Iskander short-range ballistic missile system and the Pakistani Hatf VII Babur cruise missile.

The ground chassis will comprise all the necessary components of a combat and launcher-loader vehicle. Each combat vehicle will mount two or three missiles.

Aist cruise missile is equipped with a turbofan engine for subsonic cruise missiles and unmanned aerial vehicles MS-400 produced by the Ukrainian enterprise Motor Sich. The Chinese DF-10 (CJ-10) cruise missile as well as the Pakistani Hatf VII Babur cruise missile are also equipped with this type of engine.

Specifications (with MS-400 turbofan engine)

  • maximum cruise thrust – 400 kgf;
  • fuel consumption – up to 0.8 kg/kgf;
  • diameter – 320 mm;
  • length (with extended exhaust line) – 1100 mm;
  • height (including engine mount components) – 455 mm;
  • gross empty mass – 85 kg.
  • gross launching mass – about 1500 kg;
  • combat load – 350 kg; length – 6 m;
  • diameter – 0,57 m; wingspan – 2,7 m;
  • range – 500 km; missile velocity – up to 900 km/h.

References

Шаблон:Reflist