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2.75-inch improved rocket motor

机译:2.75英寸改进型火箭发动机

摘要

The present invention relates to a 2.75 inch improved rocket motor using a double base propellant and more particularly to an improved rocket motor with a stabilized rod coating containing an intrinsic potassium salt content, Combustion instability is eliminated.;The present invention relates to a K2SO4Was used to generate ionized KOH in the motor chamber and to attach to chains with-H and-OH groups to reduce secondary combustion. It was found that the potassium salt content was increased, And increasing the outer diameter and thickness of the coating material to increase the amount of potassium salt supplied into the combustion gas per unit time.;In addition, by using the stabilizing bar of a larger dimension of coating material in the interior of the propellant (that is, the gas flow passage), the mechanical disturbance effect on the gas pulsation becomes larger, effectively suppressing the combustion instability.;Accordingly, it was possible to manufacture the 2.75 inch improved type rocket motor improved in performance by eliminating the combustion instability according to the present invention.
机译:本发明涉及一种使用双基推进剂的2.75英寸改进火箭发动机,更具体地说,涉及一种具有稳定杆涂层的改进火箭发动机,该杆涂层含有固有的钾盐含量,消除了燃烧不稳定性。 Sub> 2 SO 4 用于在发动机室中生成离子化的KOH,并连接至带有-H和-OH基团的链以减少二次燃烧。发现增加了钾盐的含量,并增加了涂层材料的外径和厚度,从而增加了单位时间内向燃烧气体中供应的钾盐的量。此外,通过使用较大的稳定杆推进剂内部(即气体流动通道)内部涂层材料的尺寸较大时,对气体脉动的机械扰动效应变大,有效地抑制了燃烧的不稳定性。因此,可以制造2.75英寸改进型通过消除根据本发明的燃烧不稳定性,改进了火箭发动机的性能。

著录项

  • 公开/公告号KR930023699A

    专利类型

  • 公开/公告日1993-12-21

    原文格式PDF

  • 申请/专利权人 오재덕;

    申请/专利号KR19920009227

  • 发明设计人 장길회;

    申请日1992-05-28

  • 分类号F42B15/00;

  • 国家 KR

  • 入库时间 2022-08-22 04:38:17

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