2005Journal of Thermal Science and TechnologyRequires access

Analysis of liquid rocket propellant evaporation characteristic in natural environment

Fengchen Zhuang

Open publisher page 3 citations

Abstract

The evaporation characteristic in the ground non-burning propellant and UDMH after the explosion of the liquid-propellant carrier rocket was studied in this paper.A theories model of the liquid rocket propellant vaporization rate in natural environment was developed.Experimental result of the evaporation rate of and UDMH in natural environment was obtained for the evaluation of harmfulness of the poisonous gas contamination of the liquid propellant rocket explosion.Its can be applied to evaluate the harmfulness of the liquid propellant rocket explosions for the space vehicle launching site.

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What this paper is about

The evaporation characteristic in the ground non-burning propellant and UDMH after the explosion of the liquid-propellant carrier rocket was studied in this paper.A theories model of the liquid rocket propellant vaporization rate in natural environment was developed.Experimental result of the evaporation rate of and UDMH in natural environment was obtained for the evaluation of harmfulness of the poisonous gas contamination of the liquid propellant rocket explosion.Its can be applied to evaluate the harmfulness of the liquid propellant rocket explosions for the space vehicle launching site.

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Available abstract

The evaporation characteristic in the ground non-burning propellant and UDMH after the explosion of the liquid-propellant carrier rocket was studied in this paper.A theories model of the liquid rocket propellant vaporization rate in natural environment was developed.Experimental result of the evaporation rate of and UDMH in natural environment was obtained for the evaluation of harmfulness of the poisonous gas contamination of the liquid propellant rocket explosion.Its can be applied to evaluate the harmfulness of the liquid propellant rocket explosions for the space vehicle launching site.

Key concepts: Propellant, Rocket propellant, Liquid-propellant rocket, Rocket (weapon), Evaporation, Aerospace engineering, Vaporization, Materials science

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