Search Results - "Ren, Quanbin"
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Tuning the Ballistic Performance of a Single-Burning-Rate Grain Solid Rocket Motor via New Discontinuous Embedded Metal Wires
Published in Aerospace (01-04-2024)“…This work proposes a new effective method to realize variable thrust through discontinuous embedded metal wires in the solid rocket motor (SRM). We aimed to…”
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Effects of Wire-Wrapping Patterns and Low Temperature on Combustion of Propellant Embedded with Metal Wire
Published in Aerospace (01-08-2024)“…Incorporating silver wires into propellant has emerged as a highly effective strategy for enhancing propellant burning rates, a technique extensively deployed…”
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A highly stretchable and self-healing hydroxy-terminated polybutadiene elastomer
Published in Journal of Saudi Chemical Society (01-12-2020)“…The damage such as microcracks limits the application of hydroxy-terminated polybutadiene (HTPB) elastomer. Here, hydroxy-carboxy-terminated polybutadiene…”
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A Study on Ultra-Low-Pressure Ratio Technology on the Basis of 3D-Printed Propellant for a Solid Rocket Motor
Published in Aerospace (01-10-2023)“…Fused deposition technology (FDM), as an additive manufacturing (AM) technology, holds immense potential in the field of solid grain manufacturing. It can…”
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Cooperative Midcourse Guidance Law with Communication Delay
Published in International journal of aerospace engineering (2021)“…The initial conditions of the cooperative terminal guidance law, which are the terminal conditions of the cooperative midcourse guidance, have a greater impact…”
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Highly Stretchable and Transparent Conductive Electrodes for Resistive Strain Sensors
Published in Macromolecular symposia. (01-06-2022)“…Conductive organic materials are a crucial component of resistive strain sensors because phase separation limits the concentration of inorganic materials in…”
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Structural response analysis of a solid rocket motor with HTPB propellant grain under vertical storage condition
Published in Xibei Gongye Daxue Xuebao (01-02-2022)“…Aiming at the structural response characteristics of solid rocket motor (SRM) under vertical storage conditions, the creep tests of HTPB propellant under…”
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