Abstract
Solid propellant grain reverse design aims to discover optimal grain geometries by shape optimization methods to match the desired solid motor performance curves. To maximize the performance matching degree and the propellant loading fraction simultaneously, this study develops a multi-objective evolutionary neural network for the grain reverse design, where the burning surface regression calculation is efficiently employed using the fast-sweeping method. Then, grain shape feature extraction and pattern analysis are achieved through image singular value decomposition and self-organizing mapping, respectively. Finally, the design case of a dual-thrust motor and a Mars ascent vehicle show that the method can well balance the performance-matching degree and propellant loading fraction. Moreover, without any training data set, it can generate dozens of grain shape patterns, highlighting their diversity and providing new ideas for solid rocket motor designers. Our method can offer a new pathway for the research field of solid rocket motor design.
| Original language | English |
|---|---|
| Pages (from-to) | 3914-3931 |
| Number of pages | 18 |
| Journal | AIAA Journal |
| Volume | 62 |
| Issue number | 10 |
| DOIs | |
| State | Published - 2024 |
Keywords
- Artificial Neural Network
- Genetic Algorithm
- Grain Design
- Optimization Algorithm
- Shape Optimization
- Solid Propellants
- Solid Rocket Motor
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