Applications of Optimization Techniques for Solid Rocket Design
DOI:
https://doi.org/10.54097/hset.v38i.5936Keywords:
Solid Rocket, Optimization Design, Hybrid Method.Abstract
Solid Rocket Motors (SRM) are rocket motors that use solid propellants (fuel/oxidizer). Optimization of the motor’s design is the process to alter the schematics of the engine for higher engine efficiency and cost minimization. Solid Rocket Motor optimization is one of the key topics of aerospace engineering research today. Conventional methods for optimization have fallen obsolete due to the exceedingly large number of design variable in modern rocket engine optimization. This paper will summarize and review some of the related research carried out in this field. Modern methods of optimization are usually designed to be multidisciplinary using complex computerized hyper-heuristic algorithms like Genetic Algorithms, sequential quadratic programming, particle swarm optimization. In conclusion, this paper could be a useful reference for those who would like to acquire a scan of the field of modern SRM optimization, learn the core methodologies for the optimization process and understand the logic of related methods.
Downloads
References
Kamran, et al. “Design and Optimization of Solid Rocket Motor Finocyl Grain Using Simulated Annealing.” Undefined, 2011, www.semanticscholar.org/paper/Design-and-optimization-of-solid-rocket-motor-grain-Kamran-Liang/1bd5835b2044ea3ca25cbca1b115f6b8075080c3. Accessed 5 Oct. 2022.
Dong-Hui, Wang, et al. “An Integrated Framework for Solid Rocket Motor Grain Design Optimization.” Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering, vol. 228, no. 7, 14 May 2013, pp. 1156–1170, 10.1177/0954410013486589. Accessed 5 Oct. 2022.
Zeping, Wu, et al. “Solid-Rocket-Motor Performance-Matching Design Framework.” Journal of Spacecraft and Rockets, vol. 54, no. 3, May 2017, pp. 698–707, 10.2514/1.a33655.
Kamm, Yair, and Alon Gany. “Solid Rocket Motor Optimization.” 44th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit, 21 July 2008, 10.2514/6.2008-4695. Accessed 5 Oct. 2022.
Hartfield, Roy, et al. “A Review of Analytical Methods for Solid Rocket Motor Grain Analysis.” 39th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit, 26 June 2003, 10.2514/6.2003-4506. Accessed 5 Oct. 2022.
Mahjub, Ahmed, et al. “Design Optimization of Solid Rocket Propulsion: A Survey of Recent Advancements.” Journal of Spacecraft and Rockets, vol. 57, no. 1, Jan. 2020, pp. 3–11, 10.2514/1.a34594.
Tola, Ceyhun, and Melike Nikbay. “Solid Rocket Motor Propellant Optimization with Coupled Internal Ballistic–Structural Interaction Approach.” Journal of Spacecraft and Rockets, vol. 55, no. 4, July 2018, pp. 936–947, 10.2514/1.a34066. Accessed 16 Apr. 2020.
Nisar, Khurram, et al. “A Hybrid Optimization Approach for SRM FINOCYL Grain Design.” Chinese Journal of Aeronautics, vol. 21, no. 6, Dec. 2008, pp. 481–487, 10.1016/s1000-9361(08)60164-8. Accessed 12 June 2021.
Rafique, Amer Farhan, et al. “Hyper Heuristic Approach for Design and Optimization of Satellite Launch Vehicle.” Chinese Journal of Aeronautics, vol. 24, no. 2, 1 Apr. 2011, pp. 150–163, www.sciencedirect.com/science/article/pii/S1000936111600198#:~:text=Hyper%20heuristic%20approach%20%28HHA%29%20based%20on%20meta-heuristics%20is, 10.1016/S1000-9361(11)60019-8. Accessed 5 Oct. 2022.
Dupont, C., et al. “New Strategy to Preliminary Design Space Launch Vehicle Based on a Dedicated MDO Platform.” Acta Astronautica, vol. 158, May 2019, pp. 103–110, 10.1016/j.actaastro.2018.04.013. Accessed 3 May 2019.
Downloads
Published
Issue
Section
License

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







