Effect of oxidizers in magnesium fuel-rich propellant for water-ramjet engine

Mei Shuai Zou; Xiao Yan Guo; Rong Jie Yang; Long Xin Qin; Zhi Hong Cheng

Effect of oxidizers in magnesium fuel-rich propellant for water-ramjet engine

Mei Shuai Zou^*, Xiao Yan Guo, Rong Jie Yang, Long Xin Qin, Zhi Hong Cheng

^*此作品的通讯作者

材料学院

Beijing Institute of Technology

科研成果: 期刊稿件 › 文章 › 同行评审

4 引用（Scopus）

摘要

The reaction thermodynamic parameters of magnesium with oxidizers(NaNO₃, KNO₃, NH₄ClO₄, KClO₄) were calculated. The burning rates were measured. Reactivities of combustion products of the propellants with sea water were studied by a method for collecting gaseous products of H₂. The results showed that the first combustion product of NH₄ClO₄ formulation has got the highest temperature, the lest residual magnesium, and lowest burning rate. The burning rate of NaNO₃ system was highest. The reaction of first combustion product of KClO₄ system with water had the largest amount of total H₂ gas. The first combustion product of NH₄ClO₄ system had the fastest reaction with sea water.

源语言	英语
页（从-至）	773-776+782
期刊	Tuijin Jishu/Journal of Propulsion Technology
卷	31
期	6
出版状态	已出版 - 12月 2010

其它文件与链接

链接到 Scopus 的出版物

引用此

@article{a02910982af1411f947307a7de21af49,

title = "Effect of oxidizers in magnesium fuel-rich propellant for water-ramjet engine",

abstract = "The reaction thermodynamic parameters of magnesium with oxidizers(NaNO3, KNO3, NH4ClO4, KClO4) were calculated. The burning rates were measured. Reactivities of combustion products of the propellants with sea water were studied by a method for collecting gaseous products of H2. The results showed that the first combustion product of NH4ClO4 formulation has got the highest temperature, the lest residual magnesium, and lowest burning rate. The burning rate of NaNO3 system was highest. The reaction of first combustion product of KClO4 system with water had the largest amount of total H2 gas. The first combustion product of NH4ClO4 system had the fastest reaction with sea water.",

keywords = "Burning rate, Combustion temperature, Hydroreactive metal fuel, Oxidizer, Reactivity",

author = "Zou, {Mei Shuai} and Guo, {Xiao Yan} and Yang, {Rong Jie} and Qin, {Long Xin} and Cheng, {Zhi Hong}",

year = "2010",

month = dec,

language = "English",

volume = "31",

pages = "773--776+782",

journal = "Tuijin Jishu/Journal of Propulsion Technology",

issn = "1001-4055",

publisher = "Journal of Propulsion Technology",

number = "6",

}

TY - JOUR

T1 - Effect of oxidizers in magnesium fuel-rich propellant for water-ramjet engine

AU - Zou, Mei Shuai

AU - Guo, Xiao Yan

AU - Yang, Rong Jie

AU - Qin, Long Xin

AU - Cheng, Zhi Hong

PY - 2010/12

Y1 - 2010/12

N2 - The reaction thermodynamic parameters of magnesium with oxidizers(NaNO3, KNO3, NH4ClO4, KClO4) were calculated. The burning rates were measured. Reactivities of combustion products of the propellants with sea water were studied by a method for collecting gaseous products of H2. The results showed that the first combustion product of NH4ClO4 formulation has got the highest temperature, the lest residual magnesium, and lowest burning rate. The burning rate of NaNO3 system was highest. The reaction of first combustion product of KClO4 system with water had the largest amount of total H2 gas. The first combustion product of NH4ClO4 system had the fastest reaction with sea water.

AB - The reaction thermodynamic parameters of magnesium with oxidizers(NaNO3, KNO3, NH4ClO4, KClO4) were calculated. The burning rates were measured. Reactivities of combustion products of the propellants with sea water were studied by a method for collecting gaseous products of H2. The results showed that the first combustion product of NH4ClO4 formulation has got the highest temperature, the lest residual magnesium, and lowest burning rate. The burning rate of NaNO3 system was highest. The reaction of first combustion product of KClO4 system with water had the largest amount of total H2 gas. The first combustion product of NH4ClO4 system had the fastest reaction with sea water.

KW - Burning rate

KW - Combustion temperature

KW - Hydroreactive metal fuel

KW - Oxidizer

KW - Reactivity

UR - http://www.scopus.com/inward/record.url?scp=79952473434&partnerID=8YFLogxK

M3 - Article

AN - SCOPUS:79952473434

SN - 1001-4055

VL - 31

SP - 773-776+782

JO - Tuijin Jishu/Journal of Propulsion Technology

JF - Tuijin Jishu/Journal of Propulsion Technology

IS - 6

ER -

Effect of oxidizers in magnesium fuel-rich propellant for water-ramjet engine

摘要

其它文件与链接

指纹

引用此