Experimental study on ignition and combustion performance of Mg/CO2

Fang Li; Chun Bo Hu; Guo Qiang He; Yi Hua Xu

Experimental study on ignition and combustion performance of Mg/CO₂

Fang Li, Chun Bo Hu, Guo Qiang He, Yi Hua Xu

School of Astronautics

Northwestern Polytechnical University Xian

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

2 Scopus citations

Abstract

The ignition performance of Mg and CO₂ was studied by a self-designed experimental device. The ignition phenomena of the reaction Mg and CO₂ was clearly exhibited by kinescope, which provided the checkout of temperature curve and also validated the combustion mode of the Mg and CO₂. The ignition temperature of reaction of Mg and CO₂ was confirmed, middling scale Mg was ignited at 960 K and the change law that the temperature is raised as the increase of particle diameter is revealed.

Original language	English
Pages (from-to)	193-196
Number of pages	4
Journal	Guti Huojian Jishu/Journal of Solid Rocket Technology
Volume	34
Issue number	2
State	Published - Apr 2011

Keywords

Ignition and combustion
Particle diameter
Powdered rocket engine
Temperature change

Cite this

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title = "Experimental study on ignition and combustion performance of Mg/CO2",

abstract = "The ignition performance of Mg and CO2 was studied by a self-designed experimental device. The ignition phenomena of the reaction Mg and CO2 was clearly exhibited by kinescope, which provided the checkout of temperature curve and also validated the combustion mode of the Mg and CO2. The ignition temperature of reaction of Mg and CO2 was confirmed, middling scale Mg was ignited at 960 K and the change law that the temperature is raised as the increase of particle diameter is revealed.",

keywords = "Ignition and combustion, Particle diameter, Powdered rocket engine, Temperature change",

author = "Fang Li and Hu, {Chun Bo} and He, {Guo Qiang} and Xu, {Yi Hua}",

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AU - Hu, Chun Bo

AU - He, Guo Qiang

AU - Xu, Yi Hua

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N2 - The ignition performance of Mg and CO2 was studied by a self-designed experimental device. The ignition phenomena of the reaction Mg and CO2 was clearly exhibited by kinescope, which provided the checkout of temperature curve and also validated the combustion mode of the Mg and CO2. The ignition temperature of reaction of Mg and CO2 was confirmed, middling scale Mg was ignited at 960 K and the change law that the temperature is raised as the increase of particle diameter is revealed.

AB - The ignition performance of Mg and CO2 was studied by a self-designed experimental device. The ignition phenomena of the reaction Mg and CO2 was clearly exhibited by kinescope, which provided the checkout of temperature curve and also validated the combustion mode of the Mg and CO2. The ignition temperature of reaction of Mg and CO2 was confirmed, middling scale Mg was ignited at 960 K and the change law that the temperature is raised as the increase of particle diameter is revealed.

KW - Ignition and combustion

KW - Particle diameter

KW - Powdered rocket engine

KW - Temperature change

UR - http://www.scopus.com/inward/record.url?scp=79959615849&partnerID=8YFLogxK

M3 - 文章

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SN - 1006-2793

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JO - Guti Huojian Jishu/Journal of Solid Rocket Technology

JF - Guti Huojian Jishu/Journal of Solid Rocket Technology

IS - 2

ER -

Experimental study on ignition and combustion performance of Mg/CO₂

Abstract

Keywords

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