Analysis of Thermal Decomposition of Solid Rocket Propellants
The paper presents results of thermal decomposition analysis of selected solid rocket propellants. Homogeneous propellant PAC and heterogeneous propellant H2 were subjected to simultaneous thermal analysis with the use of NETZSCH STA 2500 Regulus device with five heating rates of 2.5, 5, 7.5, 10 and...
| Main Authors: | , , |
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| Format: | Article |
| Language: | English |
| Published: |
Military University of Technology, Warsaw, Poland
2019-06-01
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| Series: | Problemy Mechatroniki |
| Subjects: | |
| Online Access: | http://promechjournal.pl/gicid/01.3001.0013.2115 |