|Table of Contents|

Ignition scheme of LOX/methane gas generator(PDF)

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

Issue:
2010年05期
Page:
7-12
Research Field:
研究与设计
Publishing date:

Info

Title:
Ignition scheme of LOX/methane gas generator
Author(s):
LI Chun-hong ZHANG Xiao-ping MA Dong-ying XU Hao-hai
Xi’an Aerospace Propulsion Institute, Xi’an 710100, China
Keywords:
LOX/methane gas generator ignition scheme
PACS:
V434
DOI:
-
Abstract:
The solid cartridge igniter was chosen for the ignition of LOX/methane gas generator in comparison with chemical and electric igniter. The parameters of the igniter were set by the calculation formula and experience of designing similar igniters. The time sequence of LOX/methane gas generator ignition was determined according to the characteristic of LOX/methane propellant. Four firing tests of LOX/methane gas generator were performed successfully. There was no sharp pressure peak or temperature peak appeared in the tests. The smooth ignition curve indicated that the ignition scheme was reasonable.

References:

[1]张小平, 李春红, 马冬英. 液氧/甲烷发动机动力循环方式研究[J]. 火箭推进, 2009, 35(4): 14-20. [2]禹天福, 李亚裕. 液氧/甲烷发动机的应用前景[J]. 航天

Memo

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Last Update: 1900-01-01