Heats of decomposition and explosion of double base propellants were measured as a function of aging time. They show opposite trends with aging time: heat of decomposition shows a gradual increase and heat of explosion a systematic decrease. This happens because nitroglycerin oozes out of the system during aging. The loosening of the bond between the liner and the propellant during aging was shown to be due to the contraction of the propellant which occurs on account of nitroglycerin migration from the propellant system
Calorimetric value and ignition temp. of carboxy-terminated polybutadiene$/NH_4ClO_4$ propellant dec...
© Cranfield UniversityThe manufacturing process for solventless extruded double base propellants inv...
During the storage of nitric acid ester based propellants at elevated temperatures the splitting pro...
Heats of decomposition and explosion of double base propellants were measured as a function of aging...
Heats of decomposition and explosion of double base propellants were measured as a function of aging...
Ageing behaviour, leading to ballistic changes, has been studied as a function of oxidizer loading i...
Ageing behaviour of polystyrene (PS)/ammonium perchlorate (AP) propellent leading to ballistic chang...
The ageing of double base (DB) rocket propellants is the result of chemical decomposition reactions ...
Double base propellant suffers from lack of chemical stability; this could result in self ignition d...
The ageing of double base (DB) rocket propellants, as a consequence of the chemical reactions and ph...
Thermogravimetric studies were carried out with double-base propellants to find the rate-detg. stage...
The scanning thermogram of a block sample of a double-base propellant shows a shoulder around 200°C ...
Aging studies on carboxy terminated polybutadiene (CTPB) and CTPB-based propellants have been carrie...
The safe storage time for double base propellant (DBP or DB propellant) with stabilizers could usual...
The purpose of solid propellants is to generate gas, which expands to accelerate (and spin, in the c...
Calorimetric value and ignition temp. of carboxy-terminated polybutadiene$/NH_4ClO_4$ propellant dec...
© Cranfield UniversityThe manufacturing process for solventless extruded double base propellants inv...
During the storage of nitric acid ester based propellants at elevated temperatures the splitting pro...
Heats of decomposition and explosion of double base propellants were measured as a function of aging...
Heats of decomposition and explosion of double base propellants were measured as a function of aging...
Ageing behaviour, leading to ballistic changes, has been studied as a function of oxidizer loading i...
Ageing behaviour of polystyrene (PS)/ammonium perchlorate (AP) propellent leading to ballistic chang...
The ageing of double base (DB) rocket propellants is the result of chemical decomposition reactions ...
Double base propellant suffers from lack of chemical stability; this could result in self ignition d...
The ageing of double base (DB) rocket propellants, as a consequence of the chemical reactions and ph...
Thermogravimetric studies were carried out with double-base propellants to find the rate-detg. stage...
The scanning thermogram of a block sample of a double-base propellant shows a shoulder around 200°C ...
Aging studies on carboxy terminated polybutadiene (CTPB) and CTPB-based propellants have been carrie...
The safe storage time for double base propellant (DBP or DB propellant) with stabilizers could usual...
The purpose of solid propellants is to generate gas, which expands to accelerate (and spin, in the c...
Calorimetric value and ignition temp. of carboxy-terminated polybutadiene$/NH_4ClO_4$ propellant dec...
© Cranfield UniversityThe manufacturing process for solventless extruded double base propellants inv...
During the storage of nitric acid ester based propellants at elevated temperatures the splitting pro...