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Supersonic Cruise Missiles - BrahMos

Jul 15, 2024

Supersonic Cruise Missiles: BrahMos

Brief Introduction

  • BrahMos Supersonic Cruise Missile: World's fastest cruise missile.
    • Speed: 2.8 times the speed of sound (Mach 2.8 = 1 km/s).

Components of the Missile

  • Nose Cap: Protective covering for the missile's nose.
  • Seeker: Located at the nose of the missile; crucial for target acquisition and tracking.
    • Technologies: Thermal imaging, infrared imaging, platform stabilization, high-precision inertial navigation.
  • Control System: Keeps the missile on its flight path with navigation commands.
  • Warhead: Contains explosive or toxic material to destroy the target.
  • Fuel Bladder: Stores liquid fuel.
  • Combustion Chamber: Burns the air-fuel mixture.
  • Solid Propellant: Used in the initial propulsion phase.

Guidance and Navigation

  • Two Phases: Mid-course and terminal.
    • Mid-Course: Uses inertial navigation system (INS).
    • Terminal Phase: Switches to active radar homing for higher accuracy.

Inertial Navigation System (INS)

  • Function: Uses motion and rotation sensors (gyroscopes and accelerometers).
    • Gyroscopes: Measure and maintain orientation and angular velocity (yaw, roll, pitch).
    • Accelerometers: Measure proper acceleration.
    • Autopilot Computer: Processes data and sends commands to guidance electronics to steer the missile using fins.

Active Radar Homing

  • Function: Missiles find and track targets autonomously using transmitted electromagnetic radiation.
    • Transmitter and Receiver: Emits and receives electromagnetic radiation to and from the target.
    • Measurements: Time delay, velocity, acceleration, distance, and other variables.
    • Autopilot Computer: Steers the missile based on processed data.

Propulsion System

  • Two-Stage Propulsion: Solid and liquid.
    • First Stage: Powered by solid propellant engine.
      • After ~9 seconds, solid engine falls away.
    • Second Stage: Powered by ramjet engine.

Ramjet Engine

  • Function: Uses atmospheric air at high velocity.
    • Compressed Air: Enters the combustion chamber.
    • Combustion: Fuel sprayed and ignited, producing thrust.
    • Thrust: Propels the missile to its target.

Conclusion

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