TY - JOUR
T1 - A novel controllable expansion insulation material reinforced with EMs for SRMs
T2 - Synergistic optimization mechanism of ablation resistance and thermal insulation performance
AU - Wang, Yiwei
AU - Li, Jiang
AU - Wang, Bohan
AU - Xu, Qinrui
AU - Guo, Mengfei
AU - Li, Mingjia
AU - An, Jian
N1 - Publisher Copyright:
© 2026 Elsevier Masson SAS.
PY - 2027/1
Y1 - 2027/1
N2 - To resolve that the lightweight, ablation resistance and thermal insulation of thermal insulation materials for solid rocket motors (SRMs) are difficult to synergistically improve, an innovative strategy of "high-temperature responsive controllable expansion" is proposed. Expandable microspheres (EMs) were introduced into the EPDM rubbers to prepare a new type of controllable expansion insulation material. These materials maintain a dense and continuous structure during manufacturing stages. And they can form uniform cell structure through in-situ expansion of EMs when exposed to high temperatures, realizing the dynamic synergistic improvement of thermal insulation and ablation resistance. It is shown that the EPDM-165 formula has the optimal comprehensive performance. The linear ablation rate decreases by 43.8%, the charring rate decreases by 13.4%, and the maximum backside temperature decreases by 29.5% compared with the basic formula. In the ablation motor test, the charring rate in the high-speed section is reduced by 40.7% compared with the basic formula. By controlling the formation time of the cell structure, this study effectively circumvents the problems of loose char layer and reduced ablation resistance of traditional foaming materials. It provides a new technical path for the performance breakthrough of thermal insulation materials for SRMs. It should be noted that the controllable expansion insulation materials have the limitation of performance degradation under long-term ablation conditions. And further optimization is required by improving the heat resistance of EMs and regulating the stability of the cell structure.
AB - To resolve that the lightweight, ablation resistance and thermal insulation of thermal insulation materials for solid rocket motors (SRMs) are difficult to synergistically improve, an innovative strategy of "high-temperature responsive controllable expansion" is proposed. Expandable microspheres (EMs) were introduced into the EPDM rubbers to prepare a new type of controllable expansion insulation material. These materials maintain a dense and continuous structure during manufacturing stages. And they can form uniform cell structure through in-situ expansion of EMs when exposed to high temperatures, realizing the dynamic synergistic improvement of thermal insulation and ablation resistance. It is shown that the EPDM-165 formula has the optimal comprehensive performance. The linear ablation rate decreases by 43.8%, the charring rate decreases by 13.4%, and the maximum backside temperature decreases by 29.5% compared with the basic formula. In the ablation motor test, the charring rate in the high-speed section is reduced by 40.7% compared with the basic formula. By controlling the formation time of the cell structure, this study effectively circumvents the problems of loose char layer and reduced ablation resistance of traditional foaming materials. It provides a new technical path for the performance breakthrough of thermal insulation materials for SRMs. It should be noted that the controllable expansion insulation materials have the limitation of performance degradation under long-term ablation conditions. And further optimization is required by improving the heat resistance of EMs and regulating the stability of the cell structure.
KW - Ablation resistance
KW - Controllable expansion
KW - Expandable microspheres
KW - Thermal insulation performance
KW - Thermal protection system
UR - https://www.scopus.com/pages/publications/105049068423
U2 - 10.1016/j.ast.2026.113678
DO - 10.1016/j.ast.2026.113678
M3 - Article
AN - SCOPUS:105049068423
SN - 1270-9638
VL - 180
JO - Aerospace Science and Technology
JF - Aerospace Science and Technology
M1 - 113678
ER -