首页> 外国专利> METHOD FOR MEASURING ADHESIVE STRENGTH BETWEEN ROCKET ARMOUR COATING AND THE SURFACE OF SOLID ROCKET FUEL GRAIN

METHOD FOR MEASURING ADHESIVE STRENGTH BETWEEN ROCKET ARMOUR COATING AND THE SURFACE OF SOLID ROCKET FUEL GRAIN

机译:火箭装甲涂层与固体火箭燃料颗粒表面粘结强度的测量方法。

摘要

FIELD: rocket engineering.; SUBSTANCE: method includes manufacturing of a 2-5 mm wide “sample disk” from an armoured solid rocket fuel grain and testing the said “sample disk” on a MRS-500 breaking machine. The “sample disk” is positioned in a cup-like device with inner flanging, the diameter of this flanging corresponds to the diameter of the fuel grain, and the inner diameter of the cup corresponds to the diameter of the “sample disk”. A punch pin is installed on the “sample disk”, the diameter of this punch pin corresponds to the diameter of the fuel grain. The device with the “sample disk” is installed into the operating element zone of the breaking machine and the punch pin is subjected to mechanical action “in reverse mode” while logging the diagram of fuel expulsion from the armoured coating of the “sample disk”, and the level of adhesive strength is measured by the applied expulsion force while taking into consideration the contact surface area between the solid fuel grain and the armoured coating.; EFFECT: creation of the effective method for measuring adhesive strength between the side armoured coating and the solid rocket fuel grain surface.;2 cl, 5 dwg
机译: FIELD:火箭工程。 物质:方法包括用装甲的固体火箭燃料颗粒制造2-5毫米宽的“样品盘”,并在MRS-500破碎机上测试所述“样品盘”。 “样品盘”位于带有内部凸缘的杯状装置中,该凸缘的直径对应于燃料颗粒的直径,并且杯的内径对应于“样品盘”的直径。在“样品盘”上安装了一个撞针,该撞针的直径对应于燃料颗粒的直径。将带有“样品盘”的设备安装到破碎机的操作元件区域中,并对冲头进行“反向”机械作用,同时记录“样品盘”的铠装涂层排出的燃料图;并且通过考虑到固体燃料颗粒和铠装涂层之间的接触表面积,通过施加的排出力来测量粘合强度水平。 效果:建立有效的方法来测量侧面装甲涂层与固体火箭燃料颗粒表面之间的粘合强度。; 2 cl,5 dwg

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