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Safety design and realization of hydrazine monopropellant propulsion system for satellites(PDF)

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

Issue:
2012年05期
Page:
18-23
Research Field:
研究与设计
Publishing date:

Info

Title:
Safety design and realization of hydrazine monopropellant propulsion system for satellites
Author(s):
HE Yong-ying
Shanghai Institute of Space Propulsion, Shanghai 200233, China
Keywords:
satellite;  hydrazine monopropellant propulsion system;  safety design
PACS:
V434-34
DOI:
-
Abstract:
The safety design philosophies for the existing hydrazine monopropellant propulsion systems in satellites are introduced and analyzed in the aspects of power distribution protection, fault isolation, safety margin design, etc. Implementation and validation both on ground and in orbit are also described. Several suggestions on safety design are proposed through analysis and summarization.

References:

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Memo

Memo:
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Last Update: 1900-01-01