|Table of Contents|

Research on hot tests of LOX/methane gas generator(PDF)

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

Issue:
2013年03期
Page:
21-26
Research Field:
研究与设计
Publishing date:

Info

Title:
Research on hot tests of LOX/methane gas generator
Author(s):
MA Dong-ying LU Gang ZHANG Xiao-ping LI Chun-hong
Xi’an Aerospace Propulsion Institute, Xi’an 710100, China
Keywords:
liquid rocket engine LOX/methane gas generator ignition combus
PACS:
V434-34
DOI:
-
Abstract:
Hot firing tests of LOX/methane gas generator were researched for the characteristic of ignition and combustion of LOX/methane. In this paper, the testing apparatus, scheme and situation of LOX/methane gas generator for hot firing test were described, and the test results were analyzed. The tests results indicate that the design scheme and ignition procedure of the gas generator were feasible. The gas generator can work in a wide range of pressure and mixture ratio, and had rational combustion, good temperature uniformity and a little coking.

References:

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