发明名称 |
NOZZLE DEVICE EXPOSED IN HIGH TEMPERATURE AND HIGH VELOCITY GAS AND ROCKET HAVING THE SAME |
摘要 |
PURPOSE: A nozzle device in high-temperature and high-velocity gas and a rocket having the same are provided to prevent a coating unit from becoming separated from a nozzle unit through a cover unit which covers the gap between the nozzle unit and the coating unit. CONSTITUTION: A nozzle device in high-temperature and high-velocity gas comprises a nozzle unit(141), a coating unit(142), and a cover unit(143). One end of the nozzle unit is connected to a combustion chamber of a propellant, and the other end is toward the outside. The nozzle unit is made of a titanium alloy. The coating unit is made of a ceramic material. The inner surface of the nozzle unit is coated with the coating unit. The cover unit covers a gap between the inner surface of the nozzle unit and the coating unit to prevent the coating unit from becoming separated from the nozzle unit.
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申请公布号 |
KR20120027864(A) |
申请公布日期 |
2012.03.22 |
申请号 |
KR20100089673 |
申请日期 |
2010.09.13 |
申请人 |
AGENCY FOR DEFENSE DEVELOPMENT |
发明人 |
KIM, HONG KYU;SONG, YOUNG BEUM;HONG, SUNG SUK;SHIM, IN OK |
分类号 |
F02K9/97;B64G1/40;C22C14/00 |
主分类号 |
F02K9/97 |
代理机构 |
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代理人 |
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主权项 |
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地址 |
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