Characterization of Rocket Propellant Combustion Products. ChemicalCharacterization and Computer Modeling of the Exhaust Products from Four Propellant Formulations

摘要

The objective of this work was the determination of the chemical composition ofexhaust products from the firing of scaled down rocket motors at the Army Signature Characterization Facility at Arsenal, and the comparison of those results with component levels predicted by a selected computer model. Both real time and off-line sampling and analysis approaches were employed. Four types of