Test system design for small H2/O2 rocket engine

Wan Long Liu; Peng Diao; Chong Wang; Guo Zhu Liang; Xue Jun Zhang

Test system design for small H₂/O₂ rocket engine

Wan Long Liu^*
, Peng Diao
, Chong Wang
, Guo Zhu Liang
, Xue Jun Zhang

^*此作品的通讯作者

Beihang University
China Aerospace Science and Technology Corporation

科研成果: 期刊稿件 › 文章 › 同行评审

3 引用（Scopus）

摘要

The H₂/O₂ rocket engine test system has been designed based on general test requirements of small 1000N H₂/O₂ rocket engine. The design of gas feed system was introduced. The choice of the mass velocity and pipe diameter was discussed particularly. The comparison type thrust-measuring device and the computer measurement & control system have been designed. The scaling and confirmatory tests have been carried out. The test system can be used for cold flow tests and firing tests of small H₂/O₂ rocket engine under different work conditions, and can also be supervised and controlled remotely by computer with high accuracy.

源语言	英语
页（从-至）	1646-1652
页数	7
期刊	Hangkong Dongli Xuebao/Journal of Aerospace Power
卷	25
期	7
出版状态	已出版 - 7月 2010

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引用此

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title = "Test system design for small H2/O2 rocket engine",

abstract = "The H2/O2 rocket engine test system has been designed based on general test requirements of small 1000N H2/O2 rocket engine. The design of gas feed system was introduced. The choice of the mass velocity and pipe diameter was discussed particularly. The comparison type thrust-measuring device and the computer measurement \& control system have been designed. The scaling and confirmatory tests have been carried out. The test system can be used for cold flow tests and firing tests of small H2/O2 rocket engine under different work conditions, and can also be supervised and controlled remotely by computer with high accuracy.",

keywords = "Comparison type thrust-measuring, H/O rocket engine, Measure and control, Pipeline design, Test system",

author = "Liu, \{Wan Long\} and Peng Diao and Chong Wang and Liang, \{Guo Zhu\} and Zhang, \{Xue Jun\}",

year = "2010",

month = jul,

language = "英语",

volume = "25",

pages = "1646--1652",

journal = "Hangkong Dongli Xuebao/Journal of Aerospace Power",

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T1 - Test system design for small H2/O2 rocket engine

AU - Liu, Wan Long

AU - Diao, Peng

AU - Wang, Chong

AU - Liang, Guo Zhu

AU - Zhang, Xue Jun

PY - 2010/7

Y1 - 2010/7

N2 - The H2/O2 rocket engine test system has been designed based on general test requirements of small 1000N H2/O2 rocket engine. The design of gas feed system was introduced. The choice of the mass velocity and pipe diameter was discussed particularly. The comparison type thrust-measuring device and the computer measurement & control system have been designed. The scaling and confirmatory tests have been carried out. The test system can be used for cold flow tests and firing tests of small H2/O2 rocket engine under different work conditions, and can also be supervised and controlled remotely by computer with high accuracy.

AB - The H2/O2 rocket engine test system has been designed based on general test requirements of small 1000N H2/O2 rocket engine. The design of gas feed system was introduced. The choice of the mass velocity and pipe diameter was discussed particularly. The comparison type thrust-measuring device and the computer measurement & control system have been designed. The scaling and confirmatory tests have been carried out. The test system can be used for cold flow tests and firing tests of small H2/O2 rocket engine under different work conditions, and can also be supervised and controlled remotely by computer with high accuracy.

KW - Comparison type thrust-measuring

KW - H/O rocket engine

KW - Measure and control

KW - Pipeline design

KW - Test system

UR - https://www.scopus.com/pages/publications/77955992498

M3 - 文章

AN - SCOPUS:77955992498

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VL - 25

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JO - Hangkong Dongli Xuebao/Journal of Aerospace Power

JF - Hangkong Dongli Xuebao/Journal of Aerospace Power

IS - 7

ER -

Test system design for small H2/O2 rocket engine

摘要

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引用此

Test system design for small H₂/O₂ rocket engine