2008Journal of Solid Rocket TechnologyRequires access

Effect of agglomerated boron on combustion properties of fuel-rich propellants

JI Zhuang-zhou

Open publisher page 2 citations

Abstract

The effects of agglomerated boron with different particle size and coating agent on combustion properties of boron-based fuel-rich propellants were experimentally investigated.The results show that burning rate of the propellant increases,and low-pressure combustible limit decreases with the increase of particle size of agglomerated boron,moreover pressure exponent tends to decreasing;the AP and LiF coating are in favor of increasing burning rate of the propellant and decreasing low-pressure combustible limit,but unfavorable for increasing pressure exponent.

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The effects of agglomerated boron with different particle size and coating agent on combustion properties of boron-based fuel-rich propellants were experimentally investigated.The results show that burning rate of the propellant increases,and low-pressure combustible limit decreases with the increase of particle size of agglomerated boron,moreover pressure exponent tends to decreasing;the AP and LiF coating are in favor of increasing burning rate of the propellant and decreasing low-pressure combustible limit,but unfavorable for increasing pressure exponent.

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Available abstract

The effects of agglomerated boron with different particle size and coating agent on combustion properties of boron-based fuel-rich propellants were experimentally investigated.The results show that burning rate of the propellant increases,and low-pressure combustible limit decreases with the increase of particle size of agglomerated boron,moreover pressure exponent tends to decreasing;the AP and LiF coating are in favor of increasing burning rate of the propellant and decreasing low-pressure combustible limit,but unfavorable for increasing pressure exponent.

Key concepts: Propellant, Boron, Materials science, Combustion, Coating, Particle size, Particle (ecology), Composite material

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