|Table of Contents|

Investigation on the scheme of 200N LOX/M MH thrust system(PDF)

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

Issue:
2009年03期
Page:
15-20
Research Field:
研究与设计
Publishing date:

Info

Title:
Investigation on the scheme of 200N LOX/M MH thrust system
Author(s):
Zhang Zhongli
Xi'an Aerospace Propulsion Institute,Xi'an 710100,China
Keywords:
LOX/MMHthrust system
PACS:
V434.23
DOI:
-
Abstract:
The scheme of 200N LOX/MMH thrust system was investigated,and configuration parameters were gained.The heat transfer and the flow-field were analyzed.The analysis results showed that the scheme of 200N LOX/MMH thrust system was feasible.the specific impulse can reach 3 1 70m/s,which is higher than that of present used system.

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Memo

Memo:
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Last Update: 1900-01-01