The decrease of stabilizers in propellants can be much better described with a combination of fust and zero order kinetics than with first order kinetics, which represent the experimental values quite well as long as the stabilizer content is greater than about 30 % of the original content The new model considers that the content reaches zero tn a finite time. The prediction of lifetimes is better than with first order kinetics
The ageing of double base (DB) rocket propellants, as a consequence of the chemical reactions and ph...
The experimental data collected in the discontinuous mode are often used for the computation of reac...
The efficiency of the assessment and of the development of energetic materials can be increased by m...
An equation for the decrease of stabilizer content in propellants is given, which describes the meas...
A review, with 39 refs. on quant. characterization and detn. of aging of gun and solid rocket propel...
Vier zweibasige Raketenfesttreibstoffe und ein einbasi Treibladungspulver wurden hinsichtlich Stabil...
The purpose of this work was to determine the safe shelf life of single-base propellants. The kineti...
A lifetime prediction study is carried out on four triple base propellant compositions by artificial...
A mathematical formula has been derived to assess the safe life of propellants based on the rate of ...
Ageing behaviour of polystyrene (PS)/ammonium perchlorate (AP) propellent leading to ballistic chang...
Chemical, thermal and mechanical stability are important parts in the quality and safety assessment ...
Modelling aging of solid propellants mechanical propertiesModelling aging of solid propellants mecha...
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...
The purpose of this work was to determine the safe shelf life of single-base propellants. The kineti...
The ageing of double base (DB) rocket propellants, as a consequence of the chemical reactions and ph...
The experimental data collected in the discontinuous mode are often used for the computation of reac...
The efficiency of the assessment and of the development of energetic materials can be increased by m...
An equation for the decrease of stabilizer content in propellants is given, which describes the meas...
A review, with 39 refs. on quant. characterization and detn. of aging of gun and solid rocket propel...
Vier zweibasige Raketenfesttreibstoffe und ein einbasi Treibladungspulver wurden hinsichtlich Stabil...
The purpose of this work was to determine the safe shelf life of single-base propellants. The kineti...
A lifetime prediction study is carried out on four triple base propellant compositions by artificial...
A mathematical formula has been derived to assess the safe life of propellants based on the rate of ...
Ageing behaviour of polystyrene (PS)/ammonium perchlorate (AP) propellent leading to ballistic chang...
Chemical, thermal and mechanical stability are important parts in the quality and safety assessment ...
Modelling aging of solid propellants mechanical propertiesModelling aging of solid propellants mecha...
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...
The purpose of this work was to determine the safe shelf life of single-base propellants. The kineti...
The ageing of double base (DB) rocket propellants, as a consequence of the chemical reactions and ph...
The experimental data collected in the discontinuous mode are often used for the computation of reac...
The efficiency of the assessment and of the development of energetic materials can be increased by m...