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Publishing Language: Chinese

Review of parametric optimization design for solid rocket motors

Qihu WANG1, Yajun WANG2, Youbiao CHU1( ), Bofu WANG3
The Institute of Xi'an Aerospace Solid Propulsion Technology, Xi'an 710025, China
China Aerospace Science and Technology Corporation, Beijing 100048, China
Shanghai Institute of Applied Mathematics and Mechanics, Shanghai 200444, China
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Abstract

Parametric optimization serves as a crucial means for addressing the multi-dimensional, multidisciplinary, nonlinear, and strongly coupled optimization challenges in solid rocket motor design. This research first reviews the application of parametric optimization methods in motor design across five aspects: grain structural design, nozzle contour design, casing design, overall motor design, and motor optimization considering overall rocket performance. Common technical challenges and general technical routes are summarized. Second, the technical characteristics of motor parametric optimization are discussed from three perspectives: parametric structural optimization, engineering practice constraints, and aerospace digitization. Finally, it identifies five existing technical challenges in parametric optimization design for solid motor and proposes four future research directions. The development of parametric optimization design technology is of great significance for enhancing performance limits, shortening development cycles, and promoting technological innovation.

CLC number: V435;TJ763 Document code: A Article ID: 1000-6893(2026)20-133530-19

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Acta Aeronautica et Astronautica Sinica

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Cite this article:
WANG Q, WANG Y, CHU Y, et al. Review of parametric optimization design for solid rocket motors. Acta Aeronautica et Astronautica Sinica, 2026, 47(20). https://doi.org/10.7527/S1000-6893.2026.33530

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Received: 03 March 2026
Revised: 27 March 2026
Accepted: 28 April 2026
Published: 25 October 2026
© 2026 The Journal of Acta Aeronautica et Astronautica Sinica