|Table of Contents|

Advances in atomized combustion technology research of pintle injector for liquid rocket engines(PDF)

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

Issue:
2020年04期
Page:
1-13
Research Field:
专论与综述
Publishing date:

Info

Title:
Advances in atomized combustion technology research of pintle injector for liquid rocket engines
Author(s):
SHI Pu1; ZHU Guoqiang1; LI Jinxian1; HOU Xiao2
(1.Science and Technology on Combustion, Internal Flow and Thermo-Structure Laboratory, Northwestern Polytechnical University, Xi’an 710072, China; 2.China Aerospace Science and Technology Corporation, Beijing 100048, China)
Keywords:
pintle injector;  liquid rocket engine;  thrust control;  spray performance;  combustion performance
PACS:
V434
DOI:
-
Abstract:
Pintle injector has the advantages of simple structure, high reliability, stable combustion, deep throttling, face-off capability, scalablity and low cost.Throttling technology based on pintle injector is an effective method to realize thrust regulation of liquid rocket engine, which has been widely used.Based on the development and application of pintle injector and corresponding engine technology, analysis and summary of atomization performance of pintle injector, combustion performance of pintle engine were conducted.On the basis of this, some opinions and suggestions on the research direction and emphasis of pintle injector and corresponding engine technology were proposed.

References:

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Last Update: 2020-07-30