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SMALL-CALIBER ROCKET BALLISTIC BODY

机译:小口径火箭弹道机构

摘要

The present invention relates to a small-caliber rocket ballistic body comprising a ballistic body which forms to gradually narrow toward a rear side when compared with a front side, and a balancing unit formed on an outer surface of the rear side of the ballistic body to uniformly distribute a pressure when the ballistic body is launched and at the same time to regulate fluctuation during flight of the ballistic body. Stable ballistic formation is capable of being achieved even when launched from a launcher without a steel wire, and special operation forces are capable of effectively removing tempered glass when entering a building or an aircraft vehicle or help firefighters break into a glass window during a fire in a building to assist in the entry.;COPYRIGHT KIPO 2019
机译:小口径火箭弹道体技术领域本发明涉及一种小口径火箭弹道体,其包括与前侧相比向后侧逐渐变窄的弹道体,以及形成在该弹道体的后侧的外表面上的平衡单元。发射弹体时,压力均匀分布,同时调节弹体飞行过程中的波动。即使从不带钢丝的发射器发射,也能实现稳定的弹道形成,并且特殊的操作力能够在进入建筑物或飞机时有效地去除钢化玻璃,或帮助消防员在火灾中闯入玻璃窗。协助入境的建筑物.COPYRIGHT KIPO 2019

著录项

  • 公开/公告号KR20190074091A

    专利类型

  • 公开/公告日2019-06-27

    原文格式PDF

  • 申请/专利权人 HUMANS PYRO CO. LTD.;

    申请/专利号KR20170175471

  • 发明设计人 SONG MIN KYU;

    申请日2017-12-19

  • 分类号F42B12/02;F42B10/06;F42B12/72;

  • 国家 KR

  • 入库时间 2022-08-21 11:50:32

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