Mechanical characterization of composite solid rocket propellant based on hydroxy-terminated polybutadiene
This paper presents the procedure of uniaxial mechanical characterization of composite solid rocket propellant based on hydroxy-terminated polybutadiene (HTPB), whose mechanical properties strongly depend on temperature, strain rate, natural aging and accumulated damage. A method of process...
| المؤلفون الرئيسيون: | , , , , , , |
|---|---|
| التنسيق: | مقال |
| اللغة: | English |
| منشور في: |
Association of Chemical Engineers of Serbia
2016-01-01
|
| سلاسل: | Hemijska Industrija |
| الموضوعات: | |
| الوصول للمادة أونلاين: | http://www.doiserbia.nb.rs/img/doi/0367-598X/2016/0367-598X1500067G.pdf |