Abstract
High requirements are imposed on rapidly developing rocket and space technology. One of the most important requirement is the acoustic influence on the structure. In this regard, there is a need to search for methods for predicting and modeling the reaction of individual structural elements of rocket and space technology. Electric energy sources play a prominent role in creation and ensuring the operability of space and rocket technology. These sources are usually solar batteries. The frames of solar panels in the form of ultra-lightweight rigid sandwich panels made of polymer composite materials with honeycomb are most widely used. The paper presents an approach to determining the stress-strain state of solar panel during acoustic loading. The implementing approach is presented in the form of a block diagram with a detailed description of each of the four blocks highlighted below. «Input data» is the definition of the acoustic loading spectrum, material characteristics and panel shape. “Preliminary design” is the definition of the reduced characteristics of the solar panel and the definition of the method of representation the loading. «Finite-element method» is the analysis of either random vibrations or harmonics of a steady state in the package of the finite element method. “Output data” is the selection of interest data obtained from the designing by the finite element method and their subsequent analysis. The developed approach will be useful for enterprises to introduce into the structure analysis process of rocket and space technology for strength under acoustic influence.
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References
Slyvynskyi, V.I., Sanin, A.F., Kharchenko, M.E., Kondratyev, A.V.: Thermally and dimensionally stable structures of carbon-carbon laminated composites for space applications. Proc. Int. Astronaut. Cong. (IAC) 8, 5739–5751 (2014)
Slyvynskyi, V.I., Alyamovskyi, A.I., Kondratjev, A.V., Kharchenko, M.E.: Carbon honeycomb plastic as light-weight and durable structural material. In: Proceedings of the 63th International Astronautical Congress 2012, vol. 8, pp. 6519–6529 (2012)
Adams, D.O., Webb, N.J., Yarger, C.B., et al.: Multi-functional sandwich composites for spacecraft applications: an initial assessment. Report No. NASA/CR-2007–214880. NASA, Hampton (2007)
Jet Propulsion Laboratory: Solar cell and array technology for future space science missions. NASA, Pasadena (2002)
Jet Propulsion Laboratory: Solar power technologies for future planetary science missions. NASA, Pasadena (2017)
Roibás-Millán, E., Alonso-Moragón, A., Jiménez-Mateos, A.G., Pindado, S.: Testing solar panels for small-size satellites: the UPMSAT-2 mission. Meas. Sci. Technol. 28(11), 115801 (2017). https://doi.org/10.1088/1361-6501/aa85fc
Kodiyalam, S., Nagendra, S., DeStefano, J.: Composite sandwich structure optimization with application to satellite components. AIAA J. 34(3), 614–621 (1996). https://doi.org/10.2514/3.13112
Zenkert, D.: The Handbook of Sandwich Construction. Engineering Materials Advisory Services, West Midlands (1997)
Kondratiev, A.: Improving the mass efficiency of a composite launch vehicle head fairing with a sandwich structure. East. Eur. J. Enterp. Technol. 6(7), 6–18 (2019). https://doi.org/10.15587/1729-4061.2019.184551
Slyvyns’kyy, V., Gajdachuk, V., Gajdachuk, A., Slyvyns’ka, N.: Weight optimization of honeycomb structures for space applications. In: Proceedings of the 56th International Astronautical Congress, vol. 6, pp. 3611–3620 (2005). https://doi.org/10.2514/6.IAC-05-C2.3.07
Slyvyns’kyy, V., Slyvyns’kyy, M., Polyakov, N., et al.: Scientific fundamentals of efficient adhesive joint in honeycomb structures for aerospace applications. In: Proceedings of the 59th International Astronautical Congress 2008, vol. 8, pp. 5307–5314 (2008)
Slivinsky, M., Slivinsky, V., Gajdachuk, V., et al.: New possibilities of creating efficient honeycomb structures for rockets and spacrafts. In: Proceedings of the 55th International Astronautical Congress, vol. 3, pp. 1923–1932 (2004). https://doi.org/10.2514/6.IAC-04-I.3.A.10
Kondratiev, A., Gaidachuk, V.: Weight-based optimization of sandwich shelled composite structures with a honeycomb filler. East. Eur. J. Enterp. Technol. 1(1), 24–33 (2019). https://doi.org/10.15587/1729-4061.2019.154928
Clarkson, B.L.: Structural Aspects of Acoustic Loads. AGARD, Neuilly sur Seine, France (1960)
Morshed, M.M., Hansen, C.H., Zander, A.C.: Prediction of acoustic loads on a launch vehicle: non-unique source allocation method. J. Spacecraft Rock. 52(5), 1–22 (2015). https://doi.org/10.2514/1.A33204
Panda, J.: Aeroacoustics of Space Vehicles. Paper presented at Applied Modeling & Simulation (AMS) Seminar Series, NASA Ames Research Center, CA, 8 April 2014. https://www.nas.nasa.gov/assets/pdf/ams/2014/AMS_20140408_Panda.pdf. Accessed 10 July 2020
Space engineering: Spacecraft mechanical loads analysis handbook (ECSS-E-HB-32–26A). European Space Agency, Noordwijk (2013)
James, M.M., Salton, A.R., Gee, K.L., et al.: Full-scale rocket motor acoustic tests and comparisons with empirical source models. Proc. Meet. Acoust. 18(1), 040007 (2012). https://doi.org/10.1121/1.4870984
Petras, A.: Design of sandwich structures. Dissertation, Cambridge University (1998)
Jones, R.M.: Mechanics of Composite Materials, 2nd edn. Taylor & Francis, Philadelphia (1999)
Lopes, J.P.: Effects of design parameters on damping of composite materials for aeronautical applications. Dissertation, University of Beira Interior (2013)
Abbasloo, A., Maheri, M.R.: Prediction of modal damping of FRP-honeycomb sandwich panels with arbitrary geometries. Latin Am. J. Solids Struct. 14(1), 17–35 (2017). https://doi.org/10.1590/1679-78252537
Rydberg, S.: Prediction of vibrational amplitude in composite sandwich structures: Prediction and implementation of the orthotropic damping in carbon-fibre-reinforced epoxy. Master’s thesis, Chalmers University of Technology (2013)
Panigrahi, S.K.: Damping of composite material structures with bolted joints. Bachelor’s thesis, National Institute of Technology (2012)
Lavanya, K., Krishna, P.V., Sarcar, M.M.M., Sankar, H.R.: Analysis of the damping characteristics of glass fibre reinforced composite with different orientations and viscoelastic layers. Int. J. Concept. Mech. Civil Eng. 1(1), 88–92 (2013)
Butaud, P., Foltete, E., Ouisse, M.: Sandwich structures with tunable damping properties: on the use of shape memory polymer as viscoelastic core. Compos. Struct. 153, 401–408 (2016). https://doi.org/10.1016/j.compstruct.2016.06.040
Rassaian, M., Huang, Y., Lee, J., Arakawa, T.T.: Structural analysis with vibro-acoustic loads in LS-DYNA®. In: Proceedings of the 10th International LS-DYNA® Users’ Conference, pp. 45–60 (2008)
Kondratiev, A., Gaidachuk, V., Nabokina, T., Tsaritsynskyi, A.: New possibilities in creating of effective composite size-stable honeycomb structures designed for space applications. In: Nechyporuk, M., et al. (eds.) Integrated Computer Technologies in Mechanical Engineering. AISC, vol. 1113, pp. 45–59. Springer, Cham (2020). https://doi.org/10.1007/978-3-030-37618-5_5.
Blevins, R.D.: Formulas for Dynamics, Acoustics and Vibration. Wiley, Chichester (2015)
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Nesterenko, M., Kondratiev, A. (2021). Determination of the Acoustic Strength of Solar Battery Panel for Space Applications. In: Nechyporuk, M., Pavlikov, V., Kritskiy, D. (eds) Integrated Computer Technologies in Mechanical Engineering - 2020. ICTM 2020. Lecture Notes in Networks and Systems, vol 188. Springer, Cham. https://doi.org/10.1007/978-3-030-66717-7_24
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