|Table of Contents|

Research and application on seal of high-pressure sealing-plug for spacecraft(PDF)

《火箭推进》[ISSN:1672-9374/CN:CN 61-1436/V]

Issue:
2018年03期
Page:
81-86
Research Field:
测控与试验
Publishing date:

Info

Title:
Research and application on seal of high-pressure sealing-plug for spacecraft
Author(s):
YUAN Xiaoxiao SU Cuie LIU Jianying XUAN Xiaoping
Shanghai Insititute of Space Propulsion, Shanghai 201112, China
Keywords:
sealing-plug tightening torque quantization
PACS:
V431-34
DOI:
-
Abstract:
Based on the test-port form of high-pressure pipeline for Shenzhou spacecraft propulsion system, the theoretical formula of tightening torque for the sealing-plug was obtained. According to the results of theoretical calculation and finite element simulation analysis, the quantitative tightening torque of the high-pressure sealing-plug of spacecraft is recommended as [T]=(24±5)N·m combined with the empirical checking torque.. The recommended tightening torque value has been applied to the Shen-zhou-11 spacecraft and has passed the flight assessment of spacecraft.

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Last Update: 2018-06-30