一种动态模拟方法,以优化电火箭发动机的推力调节.
Tianwen Li1, Haodong He2, Nanjia Yu3,4
1School of Astronautics, Beihang University, Beijing, 100191, China.
Scientific reports
|September 26, 2025
概括
优化电动的火箭发动机推力需要同步的组件执行. 协调定时可最大限度地减少调节时间,并确保在广泛的推力范围内保持稳定的性能.
科学领域:
- 航空航天工程 航空航天工程
- 推进系统 推进系统
- 计算流体动力学的流体动力学.
背景情况:
- 电动式火箭发动机在推力向量和压缩方面具有优势.
- 精确的推力调节对于任务成功和发动机寿命至关重要.
- 在这些复杂的系统中优化短暂动态仍然是一个挑战.
研究的目的:
- 开发一个动态模拟框架,以优化电火箭发动机的推力调节.
- 调查触动时间对推力控制效率的影响.
- 分析电动,注入器和燃烧之间的短暂相互作用.
主要方法:
- 开发了一个全面的系统模型,集成了动力学,燃烧和两相流量.
- 为了动态模拟,采用了一种步进时间的数值方法.
- 该框架模拟了推力调节在20-100%的操作范围.
主要成果:
- 同步 actuation 显著减少推力调节时间.
- 氧化器的响应时间主要影响室内压力和混合物比率.
- 一个优化的时间序列有效地减轻了在深度推力过渡期间的波动.
- 对实验数据的模型验证显示出小于1.2%的错误.
结论:
- 动态模拟提供了一个可扩展的工具,用于改进电动式发动机的推力调节.
- 了解部件启动时间对于改进推进系统设计至关重要.
- 开发的框架推进了用于火箭发动机优化的计算建模.
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