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BEARING STRUTS OF TAKEOFF-AND-LANDING SHOCK ABSORBERS OF NON-EXPENDABLE SINGLE-STAGE LAUNCH VEHICLE

机译:非延伸型单阶段发射车辆的起降减震器轴承支座

摘要

FIELD: non-expendable transport space systems of new generation (type KORONA).;SUBSTANCE: proposed struts belong to takeoff-and-landing shock absorbers of non-expendable launch vehicle. Struts are subjected to repeated gas dynamic and thermal action on side of launch vehicle engines in the course of operation. Struts are made from heat-resistant material; they are telescopic in form. Struts are retractable into and are extended from launch vehicle body in the course of launching and landing. No less than three struts shall be provided in takeoff-and-landing shock absorbers of launch vehicle. Each strut withstands load no less than launch weight of launch vehicle. Service life of these struts is about 100 flights at service life margin of 25%.;EFFECT: enhanced efficiency; increased service life of struts.;1 dwg
机译:领域:新一代非消耗性运输空间系统(KORONA型);物质:拟议的支柱属于非消耗性运载工具的起降减震器。在运行过程中,支柱会在运载火箭发动机的侧面受到反复的气体动力和热作用。支柱由耐热材料制成;它们是伸缩式的。在发射和降落的过程中,支柱可缩进发射车体中并从发射车体伸出。运载火箭的起降减震器应设置不少于三个支柱。每个支柱承受的载荷不小于运载火箭的发射重量。这些支柱的使用寿命约为100个飞行,使用寿命为25%。延长了支杆的使用寿命。; 1 dwg

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