• Title/Summary/Keyword: Wing deploying mechanism

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Ground Ejection Tests for the Safe Separation Analysis of a Gliding Bomb (활공탄의 안전분리 해석을 위한 지상투하시험)

  • Lee, Kidu;Lee, Inwon;Park, Youngkun;Baek, Seungwoock;Jung, Nahyeon;Jung, Sangjun
    • Journal of the Korean Society for Aeronautical & Space Sciences
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    • v.41 no.6
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    • pp.502-508
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    • 2013
  • Various combinations of cartridge and orifice were applied for ground ejection tests of a gliding bomb model equipped with a new guidance kit. Larger diameter of orifice made larger ejection force at each of bomb racks. Normal operations of the wing deploying mechanism and the devices inside of the bomb model were confirmed. Also high speed video data showed that pitch angle of the gliding bomb varied due to the ejection force.