|Table of Contents|

Study on heat transfer of a FSO pintle injector engine head(PDF)

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

Issue:
2010年06期
Page:
6-10
Research Field:
研究与设计
Publishing date:

Info

Title:
Study on heat transfer of a FSO pintle injector engine head
Author(s):
YANG Zhen-ning ZHANG Feng ZHOU Jun
Xi’an Aerospace Propulsion Institute, Xi’an 710100, China
Keywords:
pintle injector propellant analysis of heat transfer
PACS:
V434-34
DOI:
-
Abstract:
In this paper, the heat transfer condition of a FSO(Face Shut Off) pintle injector engine head is analyzed and modeled with numerical method. The instantaneous temperature states of the propellant in the engine head during working and shut-off states are computed. The results show that the rise amplitude of the propellant temperature is small when the engine is at work, and the propellant temperature rises less than 200℃ after the engine is shut-off. The conclusions above show that the propellant in the engine head is at a safe temperature range.

References:

[1] 张育林. 变推力液体火箭发动机及其控制技术[M]. 北京:国防工业出版社, 2001. [2] 岳春国, 李进贤, 冯喜平, 等. 针栓式变推力火箭发动机技术现状与发展探索[J]. 世界科技研究与发展, 2008, 30(5): 609-612. [3] DRESSLER Gordon, BAUER J Martin. TRW pintle engine heritage and performance characteristics, AIAA 2000- 3871 [R]. USA: AIAA, 2000. [4] ELVERUM G W, STAUDHAMMER P, MILLER J, et al. The descent engine for the lunar module, AIAA 67-521[R]. USA: AIAA, 1967. [5] MUELLER Tom, DRESSLER Gordon. TRW 40 K1bfLOX /RP-1 low cost pintle engine test results, AIAA 2000-3863[R]. USA: AIAA, 2000. [6] GAVITTETC K. Testing of the 650 K1bf LOX/LH2 low cost p intle engine(LCPE), AIAA 2001-3987[R]. USA: AIAA, 2001. [7] GAVITTETC K. TRW LCPE 650 k1bf LOX/LH2 low test results, A IAA2000-3853 [R]. USA: AIAA, 2000. [8] AUSTIN B, HEISTER S. Characterization of pintle engine performance for nontoxic hypergolic bipropellants, AIAA 2002-4029 [R]. USA: AIAA, 2002. [9] 杨世铭, 陶文铨 编著. 传热学[M]. 北京: 高等教育出版社, 1998. [10] 皮茨D, 西索姆L. 传热学[M]. 葛新石, 译. 北京: 科学出版社, 2002. [11] 巴伦 I. 纯物质热化学数据手册[M]. 程乃良, 牛四通, 徐桂英, 等译. 北京: 科学出版社, 2003. [12] 周海清, 尤政, 张平. 颗粒传热增强对微型脉冲推力点火过程的影响[J]. 固体火箭技术, 2006, 29 (3): 31-34.

Memo

Memo:
-
Last Update: 1900-01-01