Analysis of a Liquid Rocket Combustion Chamber Cooling

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原文链接

NETL
IEEE

外文摘要：This paper analyzes the ablation in a liquid rocket combustion chamber's high altitude simulation tests。 Based on the characteristic of combustion chamber and the history of the malfunction， our proposed corrective measure of the chamber and relevant product reliability validation tests were conducted。 The validation tests showed that our corrective measure is feasible and relevant reliability met our requirements。 The investigation of purchased products should start during the phases of product manufacturing， especially for the design of combustion chamber cooling。

外文关键词：

AblationCombustion chamberCoolingValidation tests

作者：

Yiteng Wang

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作者单位：

Sci. & Technol. on Space Phys. Lab., Beijing, China

会议名称：

International Conference on Internet Computing for Science and Engineering

会议地点：

Harbin(CN)

会议母体文献：

2015 Eighth International Conference on Internet Computing for Science and Engineering

页码：

135-138

出版时间：

2015

DOI：

10.1109/ICICSE.2015.33