中科微点-全球专利检索

  1. Login
  2. Sign Up

Search Results

8 records (took 0.016 seconds)

    Guided missile system
    4.
    发明专利
    Guided missile system 未知

    公开(公告)号：GB2172383A

    公开(公告)日：1986-09-17

    申请号：GB8215138

    申请日：1982-05-27

    Applicant: AEROSPATIALE

    Inventor： RAYNAUD JACQUES ,  MAREE MICHEL ,  VAILLANT ROBERT ,  ANSALDI JEAN ,  GUILLOT JEAN

    IPC: F02K9/80 ,  F02K9/30 ,  F42B13/10 ,  F42B13/30

    Abstract: A missile to be launched at low speed from a tube and equipped with a propellant system of the combustible propulsive charge type is characterised in that the propulsion system (1a, 1b, 2) is determined and positioned so that it can furnish the missile I at one and the same time with axial propulsive thrust and the forces for manoeuvring under powered guidance, so that the variation of position of the centre of gravity G of the missile I along its axis L - L as a function of the combustion of the propulsive charge is such that, at the exit of the missile from tube 7, the centre of gravity G passes through the line of action of the said manoeuvring forces and so that, during flight, generative torques of aerodynamic incidence are allowed to occur producing manoeuvring forces adding to those of powered guidance. The missile may be used with an anti-tank weapon system.

Patent Agency Ranking