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Publishing Language: Chinese

Rheological properties of boron-loaded gel fuel

Yujia FENG1Zhenhua SUN1,2( )
China Airborne Missile Academy, Luoyang 471009, China
National Key Laboratory of Air-Based Information Perception and Fusion, Luoyang 471009, China
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Abstract

Boron-loaded gel fuel is an ideal propellant for limited-volume propulsion devices such as ramjets. However, its high viscosity and complex rheological properties pose significant challenges to its practical application. In this study, a novel gel fuel with 50wt% boron content was used as the research object. Based on the complex service environments in engineering applications, a series of experiments were designed to investigate the effects of shear rate change rate, constant shear duration, pre-shearing, and temperature on the viscosity of boron-loaded gel fuel. The experimental phenomena were analyzed in depth based on shear stress. The results show that under constant shear rate, the time-dependent viscosity of boron-loaded gel fuel can be accurately described by a power function with a constant term. Pre-shearing can effectively destroy the structure of the boron-loaded gel system and make it difficult to recover within a finite time. High-low temperature cycling can hardly destroy the gel structure but can reduce its structural strength. At a constant shear rate, there exists a critical temperature: below this temperature, the viscosity of the gel fuel is negatively correlated with temperature; above this temperature, the viscosity does not change significantly. Based on shear stress analysis, it is inferred that the boron-loaded gel system has a multi-level structure. Under high-low temperature cycling, the recovery ability of the secondary structure is stronger than that of the main structure.

CLC number: V235.21;TJ760 Document code: A Article ID: 1000-6893(2026)12-132822-13

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Acta Aeronautica et Astronautica Sinica

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Cite this article:
FENG Y, SUN Z. Rheological properties of boron-loaded gel fuel. Acta Aeronautica et Astronautica Sinica, 2026, 47(12). https://doi.org/10.7527/S1000-6893.2025.32822

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Received: 24 September 2025
Revised: 17 November 2025
Accepted: 30 December 2025
Published: 16 January 2026
© 2026 The Journal of Acta Aeronautica et Astronautica Sinica