Combustion Characteristic Parameter Testing and Caculating of Single-Base Propellant

Yong Kang Chen; Ming Hua Chen; Li Zhang; Ran Zhao; Jian Wen

doi:10.4028/www.scientific.net/AMR.1006-1007.185

Paper Titles

The Influence of Thermal Resistances and Nonperfect Regenerative Losses on the Performance of a Ferroelectric Ericsson Refrigerator
p.168

Spray Cooling Rate Model of Heavy Cylinder Rolling
p.173

Stress State of a Thick-Walled Cylindrical Shell under the Combined Action of Radiation and Temperature Field
p.177

Numerical Simulation on Moisture Influence to MSW Combustion
p.181

Combustion Characteristic Parameter Testing and Caculating of Single-Base Propellant
p.185

Numerical Simulation and Experimental Research of Blade Erosion in Particulate Gas Turbine
p.188

The Current Status of Development and Applications of Wave-Heated Discharge Plasma Sources
p.193

Hazard Evaluation of Carbon Steel Water Tube Boiler under Explosion Behavior
p.200

Simulation of Geometry Parameters Optimization of Diesel Engine Combustion Chamber on Passenger Vehicle
p.204

HomeAdvanced Materials ResearchAdvanced Materials Research Vols. 1006-1007Combustion Characteristic Parameter Testing and...

Combustion Characteristic Parameter Testing and Caculating of Single-Base Propellant

Abstract:

Combustion characteristics of single base propellant are tested with closed bomb. Combustion characteristic parameters are calculated through P-t curves. Gunpowder force f=974.30J·g^-1, covolume α=1.111cm³·g^-1. Laws of combustion rate are u=4.97×10^-3P^0.82 (charge density Δ₁=0.10g·cm^-3) and u=3.97×10^-³P^0.86(charge density Δ₂=0.16g·cm^-3).