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Design of remote measurement and control system for conventional propellant bunker(PDF)

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

Issue:
2014年04期
Page:
62-66
Research Field:
测控与试验
Publishing date:

Info

Title:
Design of remote measurement and control system for conventional propellant bunker
Author(s):
ZHU Dan-bo;  ZUO Ming-cong;  SHAN Lin
Xi’an Aerospace Propulsion Test Technology Institute, Xi’an 710100, China
Keywords:
remote measurement and control system;  security monitoring;  RMS design
PACS:
V434-34
DOI:
-
Abstract:
The propellant bunker provides fuel and oxidant for the rocket engine ground test. Both the fuel and oxidant are all poisonous. The fuel is flammable and explosive. A design scheme of remote measurement and control system for the propellant bunker is proposed to improve the security of propellant storage and convenience of the operation process. The system has been successfully used in the propellant bunker, and matches with the design requirements of RMS. It improved the security and the degree of automatization.

References:

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