Rocket science unveiled: A differential equation exploration of motion
Abstract
Through the perspective of differential equations, the report "Rocket Science Unveiled" explores the amazing invention of rocket propulsion. In order to study, comprehend, and forecast the behavior of rocket engines, differential equations are essential. In order to better understand and analyze this intricate anomaly, the report aims to investigate the underlying mathematics of rocket propulsion and how differential equations work. We apply the differential equation to clarify the fuel consumption and thrust generation rates. In addition, we utilize Newton's rule of motion to explain the relationship among thrust, mass, and acceleration. Working on this study allowed us to discover the anticipated outcome for both position location and spacecraft position determination. For iterative operations, we used Euler's approach because the analytical calculation of differential equations is complicated, we used Euler's method for iterative operations. Knowing the rocket's initial or previous value allows us to locate or establish its placements with ease.
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References
Abba, S. (2018). Modeling Rocket Flight Trajectory. Workshop: Teaching Computation in the Sciences Using MATLAB, Carleton College Northfield, Minnesota, USA. https://www.researchgate.net/publication/347711217_Modeling_Rocket_Flight_Trajectory
Baum, C. M., Low, S., & Sovacool, B. K. (2022). Between the sun and us: Expert perceptions on the innovation, policy, and deep uncertainties of space-based solar geoengineering. Renewable and Sustainable Energy Reviews, 158(4), 112179. https://doi.org/10.1016/j.rser.2022.112179
Capaccioli, M. (2024). The Dawn Red Moon: The Soviet Conquest of Space. Springer.
Casiano, M. J., Hulka, J. R., & Yang, V. (2010). Liquid-propellant rocket engine throttling: A comprehensive review. Journal of Propulsion and Power, 26(5), 897–923. https://doi.org/10.2514/1.49791
Chen, S.-Y., & Xia, Q.-L. (2016). A multiconstrained ascent guidance method for solid rocket‐powered launch vehicles. International Journal of Aerospace Engineering, 2016(1), 1–11. https://doi.org/10.1155/2016/6346742
Coutand, D., & Shkoller, S. (2012). Well-posedness in smooth function spaces for the moving-boundary three-dimensional compressible Euler equations in physical vacuum. Archive for Rational Mechanics and Analysis, 206(11), 515–616. https://doi.org/10.1007/s00205-012-0536-1
Cracknell, A. P., & Varotsos, C. A. (2017). Editorial and cover: Fifty years after the first artificial satellite: from sputnik 1 to envisat. Taylor & Francis. https://doi.org/10.1080/01431160701347147
Devezas, T., de Melo, F. C. L., Gregori, M. L., Salgado, M. C. V, Ribeiro, J. R., & Devezas, C. B. C. (2012). The struggle for space: Past and future of the space race. Technological Forecasting and Social Change, 79(5), 963–985. https://doi.org/10.1016/j.techfore.2011.12.006
Harvey, B., & Harvey, B. (2019). Medieval rockets to first satellites. China in Space: The Great Leap Forward, 39–66. https://doi.org/10.1007/978-3-030-19588-5_2
Katsikadelis, J. T. (2015). Derivation of Newton’s law of motion using Galileo’s experimental data. Acta Mechanica, 226(9), 3195–3204. https://doi.org/10.1007/s00707-015-1354-y
Kotze, C. (2022). Rockets and Science Fiction: A Mutual Journey. In Outer Space and Popular Culture: Influences and Interrelations, Part 2 (pp. 75–111). Springer. https://doi.org/10.1007/978-3-030-91786-9_4
Nakayama, K. (2018). Remarks on Newton’s second law for variable mass systems. European Journal of Physics, 39(5), 1–9. https://doi.org/10.1088/1361-6404/aac751
Naseri, A., Norris, S., & Subiantoro, A. (2022). Theoretical modelling and experimental investigation of the modified revolving vane expander (M-RVE). Energy Conversion and Management, 252(1), 114997. https://doi.org/10.1016/j.enconman.2021.114997
Serol, M., Ahmad, S. M., Quintas, A., & Família, C. (2023). Chemical analysis of gunpowder and gunshot residues. Molecules, 28(14), 1–25. https://doi.org/10.3390/molecules28145550
Shirshekar, S. (2022). Pioneers of Human Space Exploration (Engineers). In Handbook of Lunar Base Design and Development (pp. 1–20). Springer. https://doi.org/10.1007/978-3-030-05323-9_13-1
Spall, N. (2021). Big History and the Significance of the 1969–1972 Apollo Lunar Landings. In Expanding Worldviews: Astrobiology, Big History and Cosmic Perspectives (pp. 307–323). Springer. https://doi.org/10.1007/978-3-030-70482-7_16
Werrett, S. (2012). Technology on the Spot: The Trials of the Congreve Rocket in India in the Early Nineteenth Century. Technology and Culture, 53(3), 598–624. https://doi.org/10.1353/tech.2012.0090
Wilhelmsen, Ø., Aasen, A., Skaugen, G., Aursand, P., Austegard, A., Aursand, E., Gjennestad, M. A., Lund, H., Linga, G., & Hammer, M. (2017). Thermodynamic modeling with equations of state: present challenges with established methods. Industrial & Engineering Chemistry Research, 56(13), 3503–3515. https://doi.org/10.1021/acs.iecr.7b00317
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