An equation for the decrease of stabilizer content in propellants is given, which describes the measured consumption of stabilizers such as diphenylamine, 2-nitrodiphenylamine, acardite II and ethylcentralite very well. The equation was obtained with a kinetic formulation for the stabilizer depletion, which combines the reactions of first and zero order. According to this model, the times up to a complete consumption of the stabilizer are finite (they are infinite if the decrease is purely exponential), and can be calculated with the reaction rate constants of the model. The prediction of the life times is considerably improved. This new equation allows a normalized representation of the stabilizer decrease, which can reveal mechanistic cha...
The ageing of double base (DB) rocket propellants is the result of chemical decomposition reactions ...
During the storage of nitric acid ester based propellants at elevated temperatures the splitting pro...
The chemical stability tests currently used for propellants suffer from some drawback. In this paper...
The decrease of stabilizers in propellants can be much better described with a combination of fust a...
A mathematical formula has been derived to assess the safe life of propellants based on the rate of ...
Diphenylamine (DPA) is used for the stabilization of solid propellants based on nitrocellulose. It r...
The purpose of this work was to determine the safe shelf life of single-base propellants. The kineti...
There could be the rare case that typical stabilizers as DPA, acardite II, 2-Nitro-DPA, used to stab...
Chemical, thermal and mechanical stability are important parts in the quality and safety assessment ...
A lifetime prediction study is carried out on four triple base propellant compositions by artificial...
The purpose of this work was to determine the safe shelf life of single-base propellants. The kineti...
Abstract-- An artillery powder undergoes slow exothermic decomposition because of their nature, even...
The efficiency of the assessment and of the development of energetic materials can be increased by m...
Three different gun propellants (A5020, JA-2 or L5460, NK1074) have been investigated up to 35 years...
Double-base (DB) propellant is vulnerable to auto-catalytic decomposition reactions during storing w...
The ageing of double base (DB) rocket propellants is the result of chemical decomposition reactions ...
During the storage of nitric acid ester based propellants at elevated temperatures the splitting pro...
The chemical stability tests currently used for propellants suffer from some drawback. In this paper...
The decrease of stabilizers in propellants can be much better described with a combination of fust a...
A mathematical formula has been derived to assess the safe life of propellants based on the rate of ...
Diphenylamine (DPA) is used for the stabilization of solid propellants based on nitrocellulose. It r...
The purpose of this work was to determine the safe shelf life of single-base propellants. The kineti...
There could be the rare case that typical stabilizers as DPA, acardite II, 2-Nitro-DPA, used to stab...
Chemical, thermal and mechanical stability are important parts in the quality and safety assessment ...
A lifetime prediction study is carried out on four triple base propellant compositions by artificial...
The purpose of this work was to determine the safe shelf life of single-base propellants. The kineti...
Abstract-- An artillery powder undergoes slow exothermic decomposition because of their nature, even...
The efficiency of the assessment and of the development of energetic materials can be increased by m...
Three different gun propellants (A5020, JA-2 or L5460, NK1074) have been investigated up to 35 years...
Double-base (DB) propellant is vulnerable to auto-catalytic decomposition reactions during storing w...
The ageing of double base (DB) rocket propellants is the result of chemical decomposition reactions ...
During the storage of nitric acid ester based propellants at elevated temperatures the splitting pro...
The chemical stability tests currently used for propellants suffer from some drawback. In this paper...