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      Development of an Optimized Induction Melting System for Fabricating Paraffin Fuel Grains for Hybrid Rocket Propulsion

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          Abstract

          ABSTRACT 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 temperature control through an on/off process. Additionally, the steel used as the material for fabricating the mold facilitates a slow cooling rate, leading to the formation of homogeneous paraffin fuel units free from cracks and microfractures, which is a critical requirement for their safe application in hybrid rockets and to ensure an efficient fuel combustion. The fabricated paraffin fuel units underwent rigorous characterization of their thermal, structural, and optical properties to ensure their suitability as fuel units in a hybrid rocket engine developed for the Mexican Cabo Tuna space program.

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          Most cited references38

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          Low temperature latent heat thermal energy storage: Heat storage materials

          A. Abhat (1983)
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            Review on sustainable thermal energy storage technologies, Part I: heat storage materials and techniques

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              Latent Heat Storage Materials and Systems: A Review

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                Author and article information

                Journal
                jatm
                Journal of Aerospace Technology and Management
                J. Aerosp. Technol. Manag.
                Departamento de Ciência e Tecnologia Aeroespacial (São José dos Campos, SP, Brazil )
                2175-9146
                2024
                : 16
                : e3024
                Affiliations
                [01] San Luis Potosí orgnameUniversidad Autónoma de San Luís Potosí orgdiv1Facultad de Ciencias Mexico
                [02] San Luis Potosí orgnameUniversidad Autónoma de San Luís Potosí orgdiv1Instituto de Física Mexico
                [03] San Luis Potosí orgnameUniversidad Autónoma de San Luís Potosí orgdiv1Facultad de Ingeniería Mexico
                [04] Mineral de la Reforma orgnameUniversidad Autónoma del Estado de Hidalgo orgdiv1Instituto de Ciencias Básicas e Ingenierías orgdiv2Área Académica de Ciencias de la Tierra y Materiales Mexico
                [05] San Luis Potosí orgnameInstituto Mexicano del Espacio Ultraterrestre México
                Author information
                https://orcid.org/0000-0003-0068-4871
                https://orcid.org/0000-0003-2875-4675
                https://orcid.org/0009-0002-6815-6872
                https://orcid.org/0000-0002-8502-1569
                https://orcid.org/0000-0001-5816-847X
                https://orcid.org/0009-0009-7708-9297
                https://orcid.org/0000-0003-3541-314X
                https://orcid.org/0000-0002-6128-0873
                https://orcid.org/0000-0002-3703-8171
                Article
                S2175-91462024000100428 S2175-9146(24)01600000428
                10.1590/jatm.v16.1350
                8ca73a53-5be2-4422-af9e-356bc6ca973c

                This work is licensed under a Creative Commons Attribution 4.0 International License.

                History
                : 04 July 2024
                : 17 September 2024
                Page count
                Figures: 0, Tables: 0, Equations: 0, References: 44, Pages: 0
                Product

                SciELO Brazil


                Hybrid propellant rocket engines,Paraffins,Magnetic induction heating,Induction systems,Propellant grains

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