| 摘要: |
| 根据某火箭三子级氢氧动力系统的规模和任务剖面要求，提出相应的IVF系统方案，建立了主要组件的静态特性模型，通过静态特性仿真，获得了3种工作模式下的IVF系统的平衡参数，并进行参数影响分析、重量优势分析。结果表明，本文提出的IVF系统方案可满足某火箭三子级任务需求，与传统方案相比具有重量轻、任务适应性强的优势。 |
| 关键词: IVF 静态特性 氢氧内燃机 换热器 系统仿真 |
| 基金项目: |
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| Static Characteristics Study on Integrated Vehicle Fluid System of H2/O2 Upper Stage |
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Zhang Wanxuan Li Jinjiang Zhang Nan
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Beijing Aerospace Propulsion Institute
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| Abstract: |
| Based on the scale and mission profile of the third stage propulsion system of a certain rocket, the paper proposes an IVF system scheme and builds static characteristic model of main components. Through static characteristic simulation, the equilibrium parameters of IVF system in 3 operating modes are obtained. The parameters, influence and advantage in weight are analyzed. The result shows that the system proposed can satisfy the mission demand of the third stage of a certain rocket. The system is superior to traditional scheme in weight and mission flexibility. |
| Key words: IVF static characteristics H2/O2 IC engine heat exchanger system simulation |
