|Table of Contents|

Design of pipelines in high pressure LOX supply system(PDF)

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

Issue:
2012年06期
Page:
70-74
Research Field:
测控与试验
Publishing date:

Info

Title:
Design of pipelines in high pressure LOX supply system
Author(s):
YAN Feng
Academy of Aerospace Propulsion Technology, Xi’an 710100, China
Keywords:
liquid rocket engine high pressure LOX supply system pipeline design
PACS:
V434-34
DOI:
-
Abstract:
The high pressure LOX supply system is the important sub-system in the extruding li- quid rocket engine test stand and is the highest pressure gas-pressurized feed system in China. Some problems existing in the design of high-pressure low-temperature propulsive agent pipelines were solved through the rational pipeline arrangement, design of special supports, self compensation and pile-up heat insulation technology. This system was proved to be reliable after several times of hot fire tests and can meet the design requirements.

References:

[1]郭霄峰. 液体火箭发动机试验[M]. 北京: 宇航出版社, 1990.
[2]徐烈, 朱卫东, 汤晓英. 低温绝热与贮运技术[M]. 北京: 机械工业出版社, 1999.

Memo

Memo:
-
Last Update: 1900-01-01