2011•Journal of Projectiles.Rockets.Missiles and GuidanceRequires access

Study of Single Ignition Test of Solid Rocket Motors

Bin Wang

Abstract

By Single ignition tests to study the influence of mass of ignition powder on the ignition transient of the igniter and the flow of gas in different mass of ignition powder and the opening pressure of the nozzle closure.The results indicates that the ignition delay of the ignitor decrease with the increase of mass of ignition powder,the ignition delay of motor and the gas-filling time and the pressure in chamber is related with the mass of ignition powder and the opening pressure of the nozzle closure.

About this research paper

What this paper is about

Why it matters

A significance statement is not available in the OpenAlex record.

Key contribution

A contribution statement is not available in the OpenAlex record.

Method / approach

Method details are not available in the OpenAlex metadata.

Main findings

Findings are not separately available in the OpenAlex metadata.

Limitations

Limitations are not available in the OpenAlex metadata.

Applications

Application details are not available in the OpenAlex metadata.

Available abstract

Key concepts: Ignition system, Nozzle, Materials science, Solid-fuel rocket, IGNITOR, Minimum ignition energy, Chamber pressure, Rocket (weapon)