Add to ORKGCalorimetric value and ignition temp. of carboxy-terminated polybutadiene$/NH_4ClO_4$ propellant decrease during accelerated aging. The behavior is attributed to binder loss and condensed phase reactions in the propellant matri
The role of thermal decomposition of the binder and the oxidiser in the thermal decomposition, agein...
Heat-up times derived from studies on the ignition characteristics of a few model composite solid pr...
Ageing studies on composite rocket propellants (CRP), which are based on HTPB (hydroxyl-terminated p...
Calorimetric value and ignition temp. of carboxy-terminated polybutadiene$/NH_4ClO_4$ propellant dec...
Abstract. Calorimetric value and ignition temperature of carboxy terminated polybutadiene/ammonium p...
Calorimetric value and ignition temperature of carboxy terminated polybutadiene/ammonium perchlorate...
Aging studies on carboxy terminated polybutadiene (CTPB) and CTPB-based propellants have been carrie...
Accelerated ageing studies for three composite propellant formulations, namely polystyrene (PS)/ amm...
The effects of ageing on the properties of a complete polyvinyl chloride - dibutyl phthalate - ammon...
Thermal ageing of hydroxyl-terminated polybutadiene propellant binders was carried out at various te...
During the thermal decomposition of orthorhombic ammonium perchlorate (AP) at 230°C, where the decom...
The role of thermal decomposition of the binder and the oxidiser in the thermal decomposition, agein...
Ageing behaviour of polystyrene (PS)/ammonium perchlorate (AP) propellent leading to ballistic chang...
Heat-up times derived from studies on the ignition characteristics of a few model composite solid p...
The role of thermal decomposition of the binder and the oxidiser in the thermal decomposition, agein...
Heat-up times derived from studies on the ignition characteristics of a few model composite solid pr...
Ageing studies on composite rocket propellants (CRP), which are based on HTPB (hydroxyl-terminated p...
Calorimetric value and ignition temp. of carboxy-terminated polybutadiene$/NH_4ClO_4$ propellant dec...
Abstract. Calorimetric value and ignition temperature of carboxy terminated polybutadiene/ammonium p...
Calorimetric value and ignition temperature of carboxy terminated polybutadiene/ammonium perchlorate...
Aging studies on carboxy terminated polybutadiene (CTPB) and CTPB-based propellants have been carrie...
Accelerated ageing studies for three composite propellant formulations, namely polystyrene (PS)/ amm...
The effects of ageing on the properties of a complete polyvinyl chloride - dibutyl phthalate - ammon...
Thermal ageing of hydroxyl-terminated polybutadiene propellant binders was carried out at various te...
During the thermal decomposition of orthorhombic ammonium perchlorate (AP) at 230°C, where the decom...
The role of thermal decomposition of the binder and the oxidiser in the thermal decomposition, agein...
Ageing behaviour of polystyrene (PS)/ammonium perchlorate (AP) propellent leading to ballistic chang...
Heat-up times derived from studies on the ignition characteristics of a few model composite solid p...
The role of thermal decomposition of the binder and the oxidiser in the thermal decomposition, agein...
Heat-up times derived from studies on the ignition characteristics of a few model composite solid pr...
Ageing studies on composite rocket propellants (CRP), which are based on HTPB (hydroxyl-terminated p...