Redirecting Missle Guidance Defense

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The redirecting missle guidance defense system deploys multiple autonomous fluidic thrust vectoring jet enginge mounts that autonomously attach onto incoming warheads and missles creating different thrust patterns rendering side spin and a asymmetric net force on the incoming missile altering/controlling the missles course of direction. The self docking fluidic thrust vectoring jet engine is optimized as lightweight (less parts) to accommodate for the additional docking parts.

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  • About the Entrant

  • Name:
    Kenneth Mailloux
  • Type of entry:
    individual
  • Patent status:
    none