Abstract
A method is developed for determining the manufacturing parameters of a lattice structure used in the primary reflector of a space telescope. The braiding parameters of the lattice structure are calculated, taking account of the characteristics of the radial braiding machine and the relevant constraints. The optimal reinforcement density is determined.
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REFERENCES
Samipour, S.A., Khaliulin, V.I., and Batrakov, V.V., Development of the technology of manufacturing aerospace composite tubular elements by radial braiding, J. Mach. Manuf. Reliab., 2018, vol. 47, pp. 284–289. https://doi.org/10.3103/S1052618818030135
Carey, J., Fahim, A., and Munro, M., Predicting elastic constants of 2D-braided fiber rigid and elastomeric-polymeric matrix composites, J. Reinf. Plast. Compos., 2004, vol. 23, pp. 1845–1857.
Hasani, H., Ajeli, S., Hessami, R., and Zadhoush, A., Investigation into energy absorption capacity of composites reinforced by three-dimensional-weft knitted fabrics, J. Ind. Text., 2014, vol. 43, pp. 536–548.
Ajeli, S. and Jeddi, A.A.A., Geometrically Poisson’s ratio of the polyester double-bar warp-knitted structures on the jamming point, J. Text. Polym., 2014, vol. 2, pp. 26–30.
Carey, J., Munro, M., and Fahim, A., Regression-based model for elastic constants of 2D-braided/woven open mesh angle-ply composites, Polym. Compos., 2005, vol. 26, pp. 152–164.
Toloei, A.R., Arani, M.S., and Abaszadeh, M., A new composite algorithm for identifying the stars in the star tracker, Int. J. Comput. Appl., 2014, vol. 102, pp. 28–33.
Toloei, A.R., Zarchi, M., and Attaran, B., Application of active suspension system to reduce aircraft vibration using PID technique and bees algorithm, Int. J. Comput. Appl., 2014, vol. 98, pp. 17–24.
Vasil’ev, V.V. and Bunakov, V.A., Design axially compressed lattice composite cylindrical shells, Compos. Struct., 2000, no. 2, pp. 68–77.
Vasil’ev, V.V., Barynin, V.A., Razin, A.F., et al., Anisogrid lattice composite structures-design and application in aerospace technology, Compos. Nanostruct., 2009, no. 3, pp. 38–50.
Samipour, S.A., Khaliulin, V.I., and Batrakov, V.V., Manufacturing technology of aerospace braided lattice structures, J. Mach. Manuf. Reliab., 2020, vol. 49, no. 9, pp. 787–795.
Samipour, S.A., Khaliulin, V.I., and Batrakov, V.V., Development of the technology of manufacturing aerospace composite tubular elements by radial braiding, J. Mach. Manuf. Reliab., 2018, vol. 47, no. 3, pp. 284–289.
Samipour, S.A. and Batrakov, V.V., Determining the design parameters of braided aerospace composite lattice structures, J. Mach. Manuf. Reliab., 2022, vol. 51, no. 1, pp. 71–79.
Samipour, S.A., Batrakov, V.V., and Konstantinov, D.U., Development of a method to reduce porosity in composite structures at limited autoclave pressure, Russ. Aeronaut., 2018, vol. 61, no. 3, pp. 360–365.
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Translated by B. Gilbert
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Samipour, S.A., Batrakov, V.V. Manufacturing the Lattice Structure for the Primary Radiator of a Space Telescope. Russ. Engin. Res. 43, 35–40 (2023). https://doi.org/10.3103/S1068798X23020193
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DOI: https://doi.org/10.3103/S1068798X23020193