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本文提出了航天飞机主发动机涡轮泵的特殊限制条件。列出了涡轮泵的工作要求并讨论了为满足施以限制条件的发动机系统的性能要求而形成的机械和流体动力的设计特点。
This paper presents the special limitations of the spacecraft main engine turbo pump. The turbine pump requirements are listed and the mechanical and fluid dynamic design features developed to meet the performance requirements of the engine system subject to the constraints are discussed.