Three different gun propellants (A5020, JA-2 or L5460, NK1074) have been investigated up to 35 years by mass loss at isothermal temperatures between 30 °C and 90 °C. From these data, activation energies for the different reactions of zero order (mass loss increase up to stabilizer consumption) and first order (solvent evaporation at begin) are derived. The mass loss data are described very well by a combination of these two reactions. Stabilizer consumption has been determined by HPLC. In case of diphenylamine (DPA), several consecutive products (mononitro-DPA up to tetranitro-DPA) have been regarded also. Activation energies are in the range of energies obtained by other methods: 84 kJ/mol [A5020], 150 kJ/mol [JA-2], 100 kJ/mol [NK 1074])....
Vier zweibasige Raketenfesttreibstoffe und ein einbasi Treibladungspulver wurden hinsichtlich Stabil...
International audienceLow vulnerability gun propellants are energetics materials designed to resist ...
An equation for the decrease of stabilizer content in propellants is given, which describes the meas...
178 different mass loss curves of A5020, JA-2 and NK 1074 propellant were recorded at temperatures b...
In this work, seven different, naturally aged gun propellants and four rocket propellants have been ...
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...
The efficiency of the assessment and of the development of energetic materials can be increased by m...
peer reviewedA stabiliser is added to gun and rocket propellants to react with species responsible f...
The purpose of this work was to determine the safe shelf life of single-base propellants. The kineti...
The surveillance of gun propellants is basically performed either by an investigation into the therm...
During the storage of nitric acid ester based propellants at elevated temperatures the splitting pro...
International audienceLow vulnerability gun propellants are energetic materials designed to resist u...
Since the beginning of the seventies TNO-Prins Maurits Laboratory (TNOPML) investigates the thermal ...
Nitrocellulose (NC) based propellants are intrinsically unstable due to degradation of NC as a funct...
Vier zweibasige Raketenfesttreibstoffe und ein einbasi Treibladungspulver wurden hinsichtlich Stabil...
International audienceLow vulnerability gun propellants are energetics materials designed to resist ...
An equation for the decrease of stabilizer content in propellants is given, which describes the meas...
178 different mass loss curves of A5020, JA-2 and NK 1074 propellant were recorded at temperatures b...
In this work, seven different, naturally aged gun propellants and four rocket propellants have been ...
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...
The efficiency of the assessment and of the development of energetic materials can be increased by m...
peer reviewedA stabiliser is added to gun and rocket propellants to react with species responsible f...
The purpose of this work was to determine the safe shelf life of single-base propellants. The kineti...
The surveillance of gun propellants is basically performed either by an investigation into the therm...
During the storage of nitric acid ester based propellants at elevated temperatures the splitting pro...
International audienceLow vulnerability gun propellants are energetic materials designed to resist u...
Since the beginning of the seventies TNO-Prins Maurits Laboratory (TNOPML) investigates the thermal ...
Nitrocellulose (NC) based propellants are intrinsically unstable due to degradation of NC as a funct...
Vier zweibasige Raketenfesttreibstoffe und ein einbasi Treibladungspulver wurden hinsichtlich Stabil...
International audienceLow vulnerability gun propellants are energetics materials designed to resist ...
An equation for the decrease of stabilizer content in propellants is given, which describes the meas...