LAUNCHING PLATFORMS FOR PROJECT K-15
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Pontoon Launcher
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This launcher is designed and developed for testing of
missiles. Design by analysis approach has been adopted for final
configuration of the launcher. The material used for launcher structure is
high-strength-lowalloy (HSLA) steel. Sets of guide rails are bolted to the
container to hold the launcher. Advanced fabrication technology has been
used to ensure the desired perpendicularity, parallesim and concentricity. A
2.3 m static seal, which restricts water ingress to the bottom of the
container, has been designed and experimentally validated for extreme
hydrostatic pressure. The system has been delivered to the user and mounted
inside a pontoon.
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Platform Launcher
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Platform launcher has been designed for launching
medium range surface-to-surface missiles. It comprises a launcher structure,
a set of shock isolation systems, a set of launcher locking mechanism, a set
of special seals and a connector alignment mechanisms for connector blind
mating. The launcher structure is having precision dimensional features for
perfect interfacing with the missile and other subsystems. The structure is
made of special high strength stainless steel for a maintenance-free service
life. This material does not need any corrosion protection against any
aggressive marine environment.
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Pontoon launcher. Inside view (right)
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Salient Features
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| Canisterised Mobile Launcher | |
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The launcher is mounted on a road mobile vehicle TATRA 8 x 8 VVL. This system has been designed for road mobility only with a maximum speed up to 40 km/hr for the specific requirements of the user. The system is used for transporting the missile from the missile integration bay to the designated launch site, levelling the launch platform within the permissible tolerance, articulating the missile from horizontal to vertical within the specified perpendicular tolerance and for launching the missile. Once the missile is transported to the designated site, it can be made ready for launching within 20 min with a five member crew. Levelling of the platform and articulation of the launch beam is done by hydraulic actuators through proportional control valves. These operations can be performed either by directly operating the control valves mounted on the vehicle chassis or through an electrical control panel from a distance of 50 m. The power can be drawn, either from the vehicle engine through power take off (PTO) or from a 5 kW petrol engine mounted on the vehicle chassis. The present design caters for the specific requirements for test firing of the missiles, however, the system has the potential to be used as mobile tube launcher with some design change to increase the mobility.
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Canisterised mobile launcher |
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Salient Features
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