Thermal decomposition reaction of nitrocellulose limits safe and reliable service life of propellants. Under certain conditions it can lead to the well-known phenomena of self-ignition. It is therefore of great concern to predict whether or not a propellant will ignite under given conditions. However, the ageing of propellants is not only a safety problem. It also causes decrease of relevant propellant properties (decrease of nitrocellulose molar mass, decrease of stabiliser content, decrease of a specimen mass, change of mechanical and ballistic performance, etc.). Thus, the ageing should be quantified by measuring both the changes of these relevant properties and hazard potential as a function of time and temperature. Some thermal properties of a stable and an unstable nitrocellulose propellants were studied in this paper in order to detect and to quantify the changes observed. The thermal characterisation was carried out by using differential scanning calorimetry and thermogravimetric analysis. It was found out that some of thermal properties and thermokinetic constant of stable (non-aged) nitrocellulose propellant, and the same propellant aged up to 9 days at 100 deg C, differ significantly. At the same time, some parameters do not change significantly within the ageing period studied.
Thermal characterisation of stable and unstable nitrocellulose propellant
Thermische Charakterisierung von stabilem und instabilem Nitrocellulose-Treibmittel
2002
17 Seiten, 11 Bilder, 2 Tabellen, 10 Quellen
Conference paper
English
Unstable burning of thin solid propellant flames
AIAA | 1980
|Thermal decomposition and combustion of nitrocellulose.
AIAA | 1968
|Unstable burning in solid and liquid propellant rocket motors
Engineering Index Backfile | 1963
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