Biaxial compression mechanical properties of HTPB propellant under dynamic loading
Source abstract
Abstract
To study the biaxial compression mechanical properties of hydroxyl-terminated polybutadiene (HTPB) solid propellants under dynamic loading, biaxial compression tests were carried out at room temperature (25 °C) with the strain rate ranging from 1 to 85 s−1 using an INSTRON testing machine with a new fixture, and microcomputed tomography (micro-CT) was used to observe the meso-damage of the loaded specimens. At the same time, a comparison test with a strain rate of 0.01 s−1 was carried out using a universal material testing machine. The experimental results indicate that the biaxial compression mechanical curves show strong nonlinear characteristics under all test conditions. Moreover, the mechanical properties of the HTPB propellant in biaxial compression are significantly affected by the strain rate, and the strain rate correlation of the HTPB propellant is controlled by different mechanisms with a strain rate of 18 s−1 as the demarcation point. Finally, from the analysis of microscopic theory combined with micro-CT reconstruction results, it is clarified that the strain rate correlation of the HTPB propellant is controlled by two different ways from the mechanism and that the effect of the strain rate on the mechanical properties of the HTPB propellant is closely related to its damage mechanism.
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Research context
OpenAlex topics: Energetic Materials and Combustion · High-Velocity Impact and Material Behavior · Electromagnetic Launch and Propulsion Technology
SciVX discovery tags are terminology-based. OpenAlex topics are source-provided classifications.
Affiliations
Xi’an High-Tech Institute , 206 Staff Room, Xi’an 710025, China
Funding
The National Natural Funds in China · The Science Project of Shaanxi Province
References (27)
Show source-provided references
1. Materials · 2020 · 13 · 303110.3390/ma13133031 ↗
2. Int. J. Pressure Vessels Piping · 2013 · 1-112 · 13110.1016/j.ijpvp.2013.06.001 ↗
3. Adv. Chem. · 1969 · 88 · 18810.1021/ba-1969-0088.ch008 ↗
4. J. Propul. Power · 2003 · 19 · 39710.2514/2.6143 ↗
5. Propellants, Explos., Pyrotech. · 1999 · 24 · 22110.1002/(sici)1521-4087(199908)24:4<221::aid-prep221>3.0.co;2-u ↗
6. AIAA J. · 1963 · 1 · 211610.2514/3.2003 ↗
7. J. Mater. Sci. Technol. · 2002 · 18 · 140810.1179/026708402225007131 ↗
8. Propellants, Explos., Pyrotech · 1999 · 24 · 34910.1002/(sici)1521-4087(199912)24:6<349::aid-prep349>3.0.co;2-1 ↗
9. Polym. Test. · 2015 · 42 · 3710.1016/j.polymertesting.2015.01.005 ↗
10. Def. Technol · 2018 · 14 · 45710.1016/j.dt.2018.06.016 ↗
11. J. Eng. Mech. · 2004 · 21 · 1
12. AIP Adv. · 2021 · 11 · 03514510.1063/5.0046785 ↗
13. Polym. Test. · 2016 · 51 · 4910.1016/j.polymertesting.2016.02.007 ↗
14. Mater. Sci. Eng. · 2018 · 378 · 1200910.1088/1757-899x/378/1/012009 ↗
15. Chin. J. Energ. Mater. · 2021 · 29 · 59210.11943/CJEM2020324 ↗
16. Int. J. Solids Struct. · 2015 · 66 · 11110.1016/j.ijsolstr.2015.03.031 ↗
17. Polym. Test. · 2015 · 45 · 4710.1016/j.polymertesting.2014.08.003 ↗
18. J. Appl. Polym. Sci · 2016 · 133 · 4351210.1002/app.43512 ↗
19. Proc. R. Soc. A · 2004 · 460 · 78110.1098/rspa.2003.1188 ↗
20. 1963
21. Mech. Mater. · 2015 · 89 · 3510.1016/j.mechmat.2015.06.002 ↗
22. Exp. Mech. · 1973 · 13 · 42210.1007/bf02324886 ↗
23. J. Appl. Polym. Sci · 2015 · 132 · 4210410.1002/app.42104 ↗
24. Z. Naturforsch. A · 1958 · 13 · 1102
25. Mater. Sci. Eng. A · 2004 · 387 · 29710.1016/j.msea.2004.02.079 ↗
26. Propellants, Explos., Pyrotech. · 1999 · 24 · 11910.1002/(SICI)1521-4087(199906)24:03<119::AID-PREP119>3.0.CO;2-G ↗
27. Phys. Rev. E. · 2009 · 80 · 6130110.1103/physreve.80.061301 ↗