Propellant Optimization

Abstract

Develop optimized spherical propellant for reduced muzzle signature, fouling and chamber pressure. Cartridges containing alternate flash suppressants and deterrents will be manufactured and tested to determine optimum propellant composition.

Document Details

Document Type
Accomplishment
Publication Date
Oct 01, 2017
Source ID
295fd686ee60fb6f334188b28c0589ec

Tags

Fields of Study

  • Physics

Readers

  • Rocket Propulsion.

Related Documents