Paper
20 September 2022 Simulation and test of solid rocket motor ignition device
Zhangjie Yuwen, Bing Liu, Jihe Qu
Author Affiliations +
Proceedings Volume 12261, International Conference on Mechanical Design and Simulation (MDS 2022); 122611F (2022) https://doi.org/10.1117/12.2638772
Event: Second International Conference on Mechanical Design and Simulation (MDS 2022), 2022, Wuhan, China
Abstract
In the use of a new type of ignition device for a solid rocket motor, its case is required to have high tensile strength. The finite element software is used to simulate the structure of the ignition device, and the bearing capacity of the ignition device is evaluated and analyzed by simulating the axial tensile test loading of the ignition device. In extreme situation, there is a possibility of partial structural damage to the ignition device. According to the analysis results, the wall thickness of the device model is increased, and the revised ignition device has passed the simulation analysis and test verification. The verification results show that the tensile structural strength performance of the new ignition device meets the design requirements, and the structural strength simulation calculation method is accurate and effective, close to the experimental test. The results are of guiding significance for the design, optimization and test of the ignition device with high tensile structural strength of solid rocket engine and its similar structures.
© (2022) COPYRIGHT Society of Photo-Optical Instrumentation Engineers (SPIE). Downloading of the abstract is permitted for personal use only.
Zhangjie Yuwen, Bing Liu, and Jihe Qu "Simulation and test of solid rocket motor ignition device", Proc. SPIE 12261, International Conference on Mechanical Design and Simulation (MDS 2022), 122611F (20 September 2022); https://doi.org/10.1117/12.2638772
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KEYWORDS
Instrument modeling

3D modeling

Rockets

Analytical research

Computer aided design

Optimization (mathematics)

Finite element methods

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