超静定捆绑火箭传力试验设计方法  

THE DESIGN OF THE FORCE TRANSFER TEST FOR STATICALLY INDETERMINATE ROCKETS

作　　者：曾耀祥 王旭 范瑞祥 祁峰 邢建伟 胡鹏翔 ZENG Yaoxiang;WANG Xu;FAN Ruixiang;QI Feng;XING Jianwei;HU Pengxiang

机构地区：[1]北京宇航系统工程研究所,北京100076

出　　处：《力学与实践》2017年第3期240-244,共5页Mechanics in Engineering

摘　　要：在综合分析试验产品,边界条件,加载激励,测量可实现性等多方面因素基础上,本文设计了一套超静定捆绑火箭传力试验方法,并通过了地面验证.该设计方法能够有效验证超静定捆绑火箭内力载荷计算的准确性,具有重要的工程指导意义.Based on the comprehensive analysis of the test products,the loading force,the boundary conditions,the measurement practicability,the force transfer test for statically indeterminate rockets is designed,and validated by tests.The test design method can be used to verify the correctness of the calculation of the internal force of the statically indeterminate rocket e?ectively.

关 键 词：超静定 捆绑火箭 传力 试验设计 

分 类 号：V421[航空宇航科学与技术—飞行器设计]