Firing test study on the Mg/CO2 powdered rocket motor

Liang Yao; Chun Bo Hu; Hu Liang Xiao; Yi Hua Xu; Guo Qiang He

Firing test study on the Mg/CO₂ powdered rocket motor

Liang Yao, Chun Bo Hu, Hu Liang Xiao, Yi Hua Xu, Guo Qiang He

School of Astronautics

Northwestern Polytechnical University Xian

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

4 Scopus citations

Abstract

A powdered rocket was preliminary designed, with Mg powder as fuel and CO₂ oxidant for firing test.The results show that powder fuel can be rapidly ignited with air under certain pressure and temperature. And after air supplying was stopped, combustion of Mg/CO₂ sustained.Most of deposition on chamber wall was white MgO, and some is unburned Mg. This test may verify the feasibility of Mg/CO₂ powdered rocket motor.

Original language	English
Pages (from-to)	440-442+447
Journal	Guti Huojian Jishu/Journal of Solid Rocket Technology
Volume	34
Issue number	4
State	Published - Aug 2011

Keywords

Air assisted combustion
Ignition and combustion
Powdered rocket motor

Cite this

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title = "Firing test study on the Mg/CO2 powdered rocket motor",

abstract = "A powdered rocket was preliminary designed, with Mg powder as fuel and CO2 oxidant for firing test.The results show that powder fuel can be rapidly ignited with air under certain pressure and temperature. And after air supplying was stopped, combustion of Mg/CO2 sustained.Most of deposition on chamber wall was white MgO, and some is unburned Mg. This test may verify the feasibility of Mg/CO2 powdered rocket motor.",

keywords = "Air assisted combustion, Ignition and combustion, Powdered rocket motor",

author = "Liang Yao and Hu, {Chun Bo} and Xiao, {Hu Liang} and Xu, {Yi Hua} and He, {Guo Qiang}",

year = "2011",

month = aug,

language = "英语",

volume = "34",

pages = "440--442+447",

journal = "Guti Huojian Jishu/Journal of Solid Rocket Technology",

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T1 - Firing test study on the Mg/CO2 powdered rocket motor

AU - Yao, Liang

AU - Hu, Chun Bo

AU - Xiao, Hu Liang

AU - Xu, Yi Hua

AU - He, Guo Qiang

PY - 2011/8

Y1 - 2011/8

N2 - A powdered rocket was preliminary designed, with Mg powder as fuel and CO2 oxidant for firing test.The results show that powder fuel can be rapidly ignited with air under certain pressure and temperature. And after air supplying was stopped, combustion of Mg/CO2 sustained.Most of deposition on chamber wall was white MgO, and some is unburned Mg. This test may verify the feasibility of Mg/CO2 powdered rocket motor.

AB - A powdered rocket was preliminary designed, with Mg powder as fuel and CO2 oxidant for firing test.The results show that powder fuel can be rapidly ignited with air under certain pressure and temperature. And after air supplying was stopped, combustion of Mg/CO2 sustained.Most of deposition on chamber wall was white MgO, and some is unburned Mg. This test may verify the feasibility of Mg/CO2 powdered rocket motor.

KW - Air assisted combustion

KW - Ignition and combustion

KW - Powdered rocket motor

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M3 - 文章

AN - SCOPUS:80053961601

SN - 1006-2793

VL - 34

SP - 440-442+447

JO - Guti Huojian Jishu/Journal of Solid Rocket Technology

JF - Guti Huojian Jishu/Journal of Solid Rocket Technology

IS - 4

ER -

Firing test study on the Mg/CO₂ powdered rocket motor

Abstract

Keywords

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