To overcome the difficulties on acquiring enough fault modes from ground and flight test data, the failure process for liquid propellant rocket propulsion systems was modeled. 為克服由于試驗或飛行數據不足而無(wú)法獲取系統足夠故障模式的問(wèn)題，開(kāi)展了液體火箭推進(jìn)系統故障過(guò)程建模與計算機仿真研究工作。
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