Military Review

Russian "Blue" against the American "Trident". Infographics

9
Sea-based missiles with Sinev nuclear warheads are in service with submarines of the Dolphin-class 667RBMD, in turn, the Americans have Trident missiles equipped with Ohio submarines.


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  1. Cxnumx
    Cxnumx 28 November 2017 09: 40
    +1
    In service with the Russian Navy less than a dozen submarines ...

    doesn’t sound very good. maybe you should write "The Russian Navy is armed with enough submarines ..."?
  2. Mik13
    Mik13 28 November 2017 10: 18
    +3
    Again, some "analyst" thought of comparing a liquid rocket with a solid rocket?
    Oh well...
    1. lance
      lance 28 November 2017 12: 20
      +1
      they will always be compared and defended their advantages.
      1. Mik13
        Mik13 28 November 2017 13: 27
        +1
        Then it is necessary to compare the totality of the tactical, technical and operational characteristics.
        Because the rocket engine, in addition to the obvious advantages in the performance characteristics, has a huge number of disadvantages in operation. And the Blue product also has such a piquant feature as a wet start.
        1. Dead duck
          Dead duck 28 November 2017 23: 38
          +7
          Quote: Mik13
          besides, it also has such a piquant feature as a "wet start"

          there is a plus in this when shooting in submerged condition ... especially when launching.
          and Americans can’t afford it ...
        2. lance
          lance 29 November 2017 06: 18
          0
          you are familiar with blue. disadvantages of operating the studio
    2. omit
      omit 27 December 2017 13: 05
      0
      Mik13
      Again, some "analyst" thought of comparing a liquid rocket with a solid rocket?
      Oh well..

      Trident 2 fuel is 75% solid.
      The solid rocket propellant is used in the Trident-2 solid propellant rocket engine. Solid components — octogen, aluminum, and ammonium perchlorate — make up 75 percent of the fuel. As a binder, polyethylene glycol, nitrocellulose, nitroglycerin and hexadiisocyanate are used. The difference from Trident-1 fuel is the use of polyethylene glycol (PEG) instead of polyglycol adipate (PGA). This allowed to increase the percentage of solids from 70 to 75. The fuel was designated PEG / NG75. Joint Venture, the fuel producer, gave it the designation NEPE-75 [5] (from the English Nitrate Ester Plasticized Polyether - a polyester plasticized with nitric acid ester).
  3. omit
    omit 27 December 2017 13: 01
    +1
    Performance characteristics
    Feature UGM-133A Trident II (D5)
    Main characteristics
    Number of steps 3
    type of solid propellant motors
    Length, m 13,42
    Diameter, m 2,11
    Maximum take-off weight, kg 59 078
    The maximum thrown weight, kg 2800
    Maximum range
    with full load, km 7800
    Maximum range
    with a reduced number of blocks, km 11 300
    Type of guidance system inertial + astro correction + GPS
    CVO, m 90 with GPS
    120 with astro correction / 360 - 500 inertial
    thermonuclear warhead
    type of warhead Separable warhead
    with individual guidance blocks
    The number of warheads up to 8 W88 (475 ct)
    or up to 14 W76 (100 ct)
    Base SSBN types
    US Flag "Ohio"
    Great Britain flag Wangard
    Launch history
    Total Launches 156
    151 of them successful
    (134 in a row)
    Of these, 4 failed
    Of these, partially unsuccessful 1 [approx. 8]
    First launch January 15, 1987 [1]
    Last Launched June 9, 2010 [34]
  4. omit
    omit 27 December 2017 13: 27
    +1
    The performance characteristics of the Sinev rocket
    Maximum range: 8,300–11,547 km [24] depending on the weight cast.
    The thrown weight (mass of warheads): to 2 800 kg
    Starting weight: 40,3 tons [25]
    Type of warhead: RGCH IN:

    up to ten individual guidance units with a power of 100 kt each. [26] (under START-3, no more than 4 warheads can be installed on SLBMs)
    4 promising individual guidance units with a capacity of 500 kt each with enhanced anti-missile defense

    Accuracy (Ultimate Deviation): 500 m
    Departure Depth: 55 m
    Length: 14,8 m
    Diameter: 1,9 m
    Number of steps: 3
    First stage rod 100 t [27]