TY-3火箭电气系统电磁兼容性设计  

The Electromagnetic Compatibility Design of Electrical System for TY-3 Rocket

作　　者：彭勤素[1] 伏川惠[1] 陈轶博[1] 王懿[1] 

机构地区：[1]中国航天科技集团公司四院四十一所,西安710025

出　　处：《固体火箭技术》2001年第3期71-74,共4页Journal of Solid Rocket Technology

摘　　要：针对 TY-3微重力试验火箭电气系统在测试中出现的供电干扰、长线干扰、脱落干扰等各种干扰因素进行了电磁兼容性分析 ,提出了改进的电路设计方案 ,通过了地面综合试验的验证和飞行试验的考核。In consideration of the factor of power supply disturbance, long-line disturbance, dropping disturbance and so on in the electrical system test for TY-3 microgravity test rocket an electromagnetic compatibility analysis is performed in the paper and an advanced electrical design plan is presented, which has proved to be effective through the examination of the comprehensive ground test and the flying test.

关 键 词：探控火箭 电气系统控制 干扰 电磁兼容性 TY-3微重力试验火箭 供电干扰 长线干扰 

分 类 号：V448.1[航空宇航科学与技术—飞行器设计]