Maximum elongation degradation model and service life prediction for HTPB propellant under constant strain and chemical aging effects
To accurately predict the service life of the hydroxy-terminated polybutadiene (HTPB) propellant, in this study, we constructed a maximum elongation degradation model that comprehensively considers physical damage and chemical aging effects. Specifically, we conducted accelerated thermal aging and u...
Saved in:
| Main Authors: | Tingjing Geng, Hongfu Qiang, Heyang Miao, Xueren Wang, Zhejun Wang, Huimin Zhang |
|---|---|
| Format: | Article |
| Language: | English |
| Published: |
Elsevier
2025-02-01
|
| Series: | Polymer Testing |
| Subjects: | |
| Online Access: | http://www.sciencedirect.com/science/article/pii/S014294182500025X |
| Tags: |
Add Tag
No Tags, Be the first to tag this record!
|
Similar Items
-
Constant Strain Aging Model of HTPB Propellant Involving Thermal–Mechanical Coupled Effects
by: Pengju Qin, et al.
Published: (2025-06-01) -
Synthesis of propellant grade HHTPB by hydrogenation of HTPB using Pd-activated charcoal as catalyst
by: Ch. Devi Vara Prasad, et al.
Published: (2025-03-01) -
The Synergistic Effect of Fe-Based MOFs and HTPB on AP Decomposition in Solid Propellants
by: Qian Guo, et al.
Published: (2025-06-01) -
Experimental and simulation study on micro damage of HTPB propellant under multi angle tensile shear loading
by: Wang Jiaxiang, et al.
Published: (2025-07-01) -
Macro-microscopic study on the damage threshold strain of particle-filled polymer composites
by: Wang Jiaxiang, et al.
Published: (2025-04-01)