Noncrystalline Binder Based Composite Propellant

HTPB-Polyurethane: A Versatile Fuel Binder for Composite Solid Propellant

Noncrystalline L-Phenylalanine-Silica Hybrid Composite Materials for High Selective Reversed Phase Liquid Chromatography

A Model of Ap/htpb Composite Propellant Combustion in Rocket-motor Environments

A comprehensive theoretical/numerical model for treating AP/HTPB composite-propellant combustion in a rocket-motor environment is presented. The formulation takes into account the conservation equations in both the gas and condensed phases, and accommodates finiterate chemical kinetics and variable thermophysical properties. The processes in the two phases are coupled at the surface to determin...

To appear in “Noncrystalline materials for Optoelectronics”,

In this paper, we review some recent work on amorphous materials using current “first principles” electronic structure/molecular dynamics techniques. The main theme of the paper is to emphasize new directions in the use of such ab initio methods. Some of these, being quite new, need development, but we believe have promise for solving new and important kinds of problems in the physics of glassy...

بررسی راهکارهای بهبود خواص حرارتی و مکانیکی پلی‌یورتان‌های بر پایه گلایسیدیل آزید پلیمر(علمی-ترویجی)

Glycidyl azide polymer (GAP) is a unique elastomeric binder with high heat of formation and high density due to enhanced thermal and performance properties of composite solid propellants. However, GAP has high glass transition temperature and poor mechanical properties that are limited its application as a binder in a composite solid propellant. In this paper , the efforts carried out on modifi...