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MANUFACTURING METHOD OF COMPOSITE FOR SOLID PROPELLANT AND COMPOSITE FOR SOLID PROPELLANT BY THE METHOD

机译:该方法固体推进剂复合材料的制造方法

摘要

The present invention relates to a method for producing a solid propellant composition and a solid propellant composition prepared by the method, and the raw materials for producing the solid propellant are divided and injected into a vacuum mixer, and a vacuum mixing process is performed between each injection step, and a curing agent is added. After injecting the last of the raw materials, the final vacuum mixing process is carried out to lower the viscosity of the propellant to prevent defects such as pores or cracks in the manufactured solid propellant, improve the quality of the solid propellant, and to improve the quality of the solid propellant. It enables stable solid propellant operation by preventing rocket explosion accidents caused by
机译:本发明涉及制备固体推进剂组合物的方法和通过该方法制备的固体推进剂组合物,并将用于生产固体推进剂的原料分开并注入真空混合器中,并且在各自之间进行真空混合过程 注射步骤,加入固化剂。 在注射最后的原料后,进行最终真空混合过程以降低推进剂的粘度,以防止制造的固体推进剂中的孔或裂缝等缺陷,提高固体推进剂的质量,并改善 固体推进剂的质量。 通过防止由射箭爆炸事故引起的火箭爆炸事故实现稳定的固体推进剂操作

著录项

  • 公开/公告号KR20210155887A

    专利类型

  • 公开/公告日2021-12-24

    原文格式PDF

  • 申请/专利权人 주식회사 한화;

    申请/专利号KR1020200073352

  • 发明设计人 박성준;최성한;박정호;노태호;

    申请日2020-06-17

  • 分类号C06B21;C06B23;C06B27;

  • 国家 KR

  • 入库时间 2022-08-24 23:02:41

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