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

^*Corresponding author for this work

Research output: Contribution to journal › Article › peer-review

3 Scopus citations

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.

Original language	English
Pages (from-to)	1646-1652
Number of pages	7
Journal	Hangkong Dongli Xuebao/Journal of Aerospace Power
Volume	25
Issue number	7
State	Published - Jul 2010

Keywords

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

Cite this

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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",

issn = "1000-8055",

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number = "7",

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TY - JOUR

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

SN - 1000-8055

VL - 25

SP - 1646

EP - 1652

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

Abstract

Keywords

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