This work reports the development of an induction melting system for producing paraffin-based fuel units for hybrid rockets. The system is based in oscillating low-frequency magnetic field to generate heat within the material, enabling a precise ...
José Refugio Martínez +8 more
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Advances in Structural Reliability Analysis of Solid Propellant Grain: A Comprehensive Review. [PDF]
Tang C +4 more
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Influence of plasma-enhanced combustion on RBCC engine using URANS. [PDF]
Zhang WR, Liu YS, Zou XR, Xu C, Xue R.
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Computational study of unsteady Homann type flow of ternary hybrid nanofluid in the presence of induced magnetic forces and time relaxation. [PDF]
Ahmad L +4 more
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Modeling fatigue damage evolution in CMDB propellant based on dynamic modulus. [PDF]
Yao L +4 more
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Simulation Model for Hardware-in-the-Loop Tests of the ILR-33 AMBER Rocket Control System. [PDF]
Cieśliński D +4 more
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Design and Manufacturing of Experimental Solid Propellant Rocket Motor Cases Made of Carbon Composite Materials. [PDF]
Baiserikov B +7 more
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Metal-Carbon Synergy in C60@Ru Nanocomposite for High-Performance Hydrazine Fuel. [PDF]
Mu X, Wang J, Wang S, Zhang Y, Yang J.
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Overcoming high-temperature performance limitations: Multidimensional design and innovation of thin-film thermocouples. [PDF]
Zhang Z +9 more
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Mechanical Properties Testing and Numerical Modeling and Simulations of a Nozzle Cover Made of Expanded Polystyrene. [PDF]
Jiang J, Zhang Z, Zheng J, Shu K, Zhu W.
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