Aerospace Systems

  • Parachute systems   The cargo parachute systems MKS-350-9, MKS-350-12 are intended for air drop of armaments, military vehicles and cargo. The parachute systems, designed and developed on the basis of main parachute with area of 350 m2, allow to drop heavy cargos with mass up to 14,400 kg from different type of aircraft. Several types of parachute systems have been developed and have been in service by the present time.
  • FAE bomb   The ODAB-500PMV fuel-air-explosive bomb is designed to engage industrial facilities, soft-skinned targets, manpower, and clear anti-personnel and anti-tank minefields.
  • General-purpose HE fragmentation bomb   The OFAB-500U general-purpose HE fragmentation bomb is designed to destroy military industrial facilities, light armored and soft-skin targets, railway junctions, military fortifications, manpower. It provides above-ground, instantaneous-contact and delayed action.
  • Fragmentation high-explosive incendiary bomb   The OFZAB-500 fragmentation high-explosive incendiary bomb is designed to engage light armored and soft-skin targets, POL depots and other targets through the combined blast, fragmentation and thermal effects.
  • Practice bomb   The P-50T practice bomb is designed to train aircrews in bombing. It can be used at any time of the day.
  • Launch vehicle   The Proton-M heavy-class launch vehicle (LV) is an upgraded version of the Proton-K. The LV is able to deliver payloads directly into designated geostationary orbit points, thus making possible the insertion of satellites which are not equipped with an apogee propulsion unit. It can liftoff from launch pads currently operational at the Baikonur Cosmodrome. The Proton-M is designed as a tandem LV with transverse separation of stages. It is composed of three stages and spacehead with Breeze-M upper stage as forth stage. All stages of the LV and upper stage are fueled by hypergolic propellant components: unsymmetrical dimethyl hydrazine as fuel, and nitrogen tetroxide as oxidizer. The Proton-M has a larger payload fairing as compared with Proton-K in order to double the space available for payloads. Upgrading (replacement) of the control system enables to improve power performance as well as operational and environment characteristics of the LV. The Breeze-M upper stage enables to deliver 3-3.2 ton payloads into geostationary orbit.
  • Brake landing parachute systems   The brake landing parachute systems:
    • reduce the length of aircraft landing run in 1.5 - 2 times;
    • are reliably deployed;
    • are simple in operation;
    • have longterm total service life.
    Problems, solved on the stage of development of the brake landing parachute systems:
    • installation and deployment of parachute system at any variant of its mounting on the aircraft;
    • parachute system stable operation in aircraft wake;
    • reduced period of time of parachute system preparation for application;
    • increase of total service life of the parachute system.
  • Brake landing parachute systems   The brake landing parachute systems:
    • reduce the length of aircraft landing run in 1.5 - 2 times;
    • are reliably deployed;
    • are simple in operation;
    • have longterm total service life.
    Problems, solved on the stage of development of the brake landing parachute systems:
    • installation and deployment of parachute system at any variant of its mounting on the aircraft;
    • parachute system stable operation in aircraft wake;
    • reduced period of time of parachute system preparation for application;
    • increase of total service life of the parachute system.
  • Brake landing parachute systems   The brake landing parachute systems:
    • reduce the length of aircraft landing run in 1.5 - 2 times;
    • are reliably deployed;
    • are simple in operation;
    • have longterm total service life.
    Problems, solved on the stage of development of the brake landing parachute systems:
    • installation and deployment of parachute system at any variant of its mounting on the aircraft;
    • parachute system stable operation in aircraft wake;
    • reduced period of time of parachute system preparation for application;
    • increase of total service life of the parachute system.
  • Brake landing parachute systems   The brake landing parachute systems:
    • reduce the length of aircraft landing run in 1.5 - 2 times;
    • are reliably deployed;
    • are simple in operation;
    • have longterm total service life.
    Problems, solved on the stage of development of the brake landing parachute systems:
    • installation and deployment of parachute system at any variant of its mounting on the aircraft;
    • parachute system stable operation in aircraft wake;
    • reduced period of time of parachute system preparation for application;
    • increase of total service life of the parachute system.
  • Brake landing parachute systems   The brake landing parachute systems:
    • reduce the length of aircraft landing run in 1.5 - 2 times;
    • are reliably deployed;
    • are simple in operation;
    • have longterm total service life.
    Problems, solved on the stage of development of the brake landing parachute systems:
    • installation and deployment of parachute system at any variant of its mounting on the aircraft;
    • parachute system stable operation in aircraft wake;
    • reduced period of time of parachute system preparation for application;
    • increase of total service life of the parachute system.
  • Brake landing parachute systems   The brake landing parachute systems:
    • reduce the length of aircraft landing run in 1.5 - 2 times;
    • are reliably deployed;
    • are simple in operation;
    • have longterm total service life.
    Problems, solved on the stage of development of the brake landing parachute systems:
    • installation and deployment of parachute system at any variant of its mounting on the aircraft;
    • parachute system stable operation in aircraft wake;
    • reduced period of time of parachute system preparation for application;
    • increase of total service life of the parachute system.
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