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Military


Kamorta Project 28 ASW Corvette Specifications

Specifications
Displacement 1,800 tons - light
2500 tons - standard displacement
Length94 meters / 109.1 meters
Beam13 meters / 13.7 meters
Draft3.5 meters
Molded Depth8.5 meters
Propulsion initial design

CODAG propulsion system
  • twin gas turbines
  • twin diesel engines
  • twin diesel generators
  • two-shaft, controllable-pitch propellers

    OR - later design

    four Pielstick 12 PA6 STC engines, each rated at 4270 Kw.
    • Range4,000 nm
    Endurance 15 days
    3450 app at 18kts
    Speed 25-27 Knots,
    later design = 28-32 knots
    Armament
  • One OTOBreda Melara 76mm Super Rapid Gun Mount (SRGM)
  • one 16-cell Barak SAM (Surface-to-Air Missile) launcher
  • Two 12-barrel RBU-6000 ASW mortar launchers
  • twin ILAS triple-tube torpedo launchers
  • Franco-Italian MU-90 533mm lightweight torpedoes

    initial design included
  • eight-cell VLS Klub-N 220km-range supersonic ASCM
  • Two AK-630M CIWS (Close In Weapon System)
    • Aircraft Ka-28PL or Naval HAL Dhruv
    Crew 85



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