Results 71 to 80 of about 402 (183)

Research on microscopic structure–activity relationship of AP particle–matrix interface in HTPB propellant

e-Polymers
The matrix and particle interface of hydroxyl-terminated polybutadiene (HTPB) propellant is the weakest part of its mechanical properties, making it prone to dewetting damage and destroying the structural integrity of the propellant.
Zou Zijie, Qiang Hongfu, Zhou Junhong, Zhang Fengtao, Wang Xueren, Li Yiyi   +5 more
doaj   +1 more source

Experimental study on the porosity of HTPB propellant: characterization of damage evolution

Journal of Materials Research and Technology
To characterize the damage evolution mechanism of HTPB composite solid propellant, the porosity as well as the sphericity will be analyzed using micro-CT. Under normal temperature and pressure, the damage mechanisms include voids, ''dewetting'' damage at
Huihui Zhang, Ruyan Zhao, Zhibin Shen, Haiyang Li, Dapeng Zhang, Kuangwei Deng   +5 more
doaj   +1 more source

Mechanical properties of HTPB composite propellants in the initial period of service life [PDF]

Scientific Technical Review, 2014
Uniaxial tensile tests of different composite solid rocket propellant compositions, based on hydroxyl-terminated polybutadiene (HTPB), have shown that mechanical properties extensively change after curing, up to 100% of their initial values, during the ...
Gligorijević Nikola, Živković Saša, Subotić Sredoje, Pavković Bojan, Nikolić Momčilo, Kozomara Stevan, Rodić Vesna   +6 more
doaj  

The Synergistic Effect of Fe-Based MOFs and HTPB on AP Decomposition in Solid Propellants

Solids
Many factors and their mutual interaction between catalysts and AP/HTPB composite solid propellant induce the complexity in the combustion. Among them, we prepared two Fe-based MOFs as catalysts and investigated their catalytic effects and mechanism on ...
Qian Guo, Jie Wang, Yanchun Li, Ramón Artiaga   +3 more
doaj   +1 more source

Ultrasonically Accelerated Nitration of Hydroxyl-Terminated Polybutadiene: Process Efficiency and Product Characterization

Eng
Hydroxyl-terminated polybutadiene (HTPB) is widely studied and the most used prepolymer for the binder system of composite solid propellants. A suitable functionalization of HTPB with energetic groups greatly improves the performance of the propellant ...
Ventsislav Bakov, Spaska Yaneva, Nadezhda Rangelova, Milko Berner, Damyan Ganchev, Nikolai Georgiev   +5 more
doaj   +1 more source

Dynamic Mechanical Response and Damage Mechanism of HTPB Propellant under Impact Loading. [PDF]

Materials (Basel), 2020
Zhang H, Liu M, Miao Y, Wang H, Chen T, Fan X, Chang H.   +6 more
europepmc   +1 more source

Experimental and simulation study on micro damage of HTPB propellant under multi angle tensile shear loading

Polymer Testing
The damage evolution of composite solid propellants is influenced by the stress state. In order to investigate the in-situ damage evolution mechanism of hydroxyl terminated polybutadiene (HTPB) propellant under tensile shear conditions, computer ...
Wang Jiaxiang, Qiang Hongfu, Pei Shudi, Li Shiqi   +3 more
doaj   +1 more source

Investigation of hydroxyl-terminated polybutadiene propellant breaking characteristics and mechanism impacted by submerged cavitation water jet

Defence Technology
A submerged cavitation water jet (SCWJ) is an effective method to recycle solid propellant from obsolete solid engines by the breaking method. Solid propellant’s breaking modes and mechanical process under SCWJ impact are unclear.
Wenjun Zhou, Meng Zhao, Bo Liu, Youzhi Ma, Youzhi Zhang, Xuanjun Wang   +5 more
doaj   +1 more source

Hydroxyl-terminated polybutadiene liner curing process monitoring using non-collinear ultrasonic wave mixing technique

AIP Advances
The Hydroxyl-Terminated Polybutadiene (HTPB) liner in solid rocket motors is a viscoelastic material formed through the polymerization and gelation of HTPB and toluene diisocyanate.
Dawei Wang, Yuxin Xie, Xinyi Gao
doaj   +1 more source

Curing Properties of HTPB-based Solid Propellants

Journal of the Korean Society of Propulsion Engineers, 2022
Su-A Jeon, Jee-Hun Ahn, Hang-seok Seo, Han-Jun Kim, Eui-yong Park   +4 more
openaire   +1 more source