Ignition and Combustion Performance for Coal-Based High Energy Kerosene

被引：0
|
作者：
Xu H.-B. [1 ,2 ]
Zhang Q.-Z. [3 ]
Zeng Y.-M. [1 ,2 ]
Yang J. [3 ]
Jin S.-Y. [1 ,2 ]
机构：
[1] Shanghai Institute of Space Propulsion, Shanghai
[2] Shanghai Engineering Research Center of Space Engine, Shanghai
[3] Shanghai Institute of Organic Chemistry, Chinese Academy of Sciences, Shanghai
来源：
Tuijin Jishu/Journal of Propulsion Technology | 2022年 / 43卷 / 04期
关键词：
Coal-based high energy kerosene; Combustion performance; Response performance; Rocket kerosene; Vacuum specific impulse;
D O I：
10.13675/j.cnki.tjjs.200660
中图分类号：
学科分类号：
摘要：
Firing-tests of attitude control engine for GOX/kerosene were carried out to study the iginition and combustion characteristics of coal-based high energy kerosene. The vacuum specific impulse, pulse operation performance, response performance of coal-based high energy kerosene engine were studied. Results show that the engine has reliable ignition and stable combustion performance by using the coal-based high energy kerosene. The pulse operation performance, starting and shut off response performance could satisfy the engineering application requirements. The vacuum specific impulse is 7s higher than that of the basic rocket kerosene engine. © 2022, Editorial Department of Journal of Propulsion Technology. All right reserved.
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