Numerical simulations of the transpiration cooling thruster with a four-section porous wall show that the design reduces of the required coolant flow by half.
对分四段结构喷管的数值模拟的结果表明，相比不分段而言分段结构可减少一半冷却剂流量。
Numerical simulations of the transpiration cooling thruster with a four-section porous wall show that the design reduces of the required coolant flow by half.
对分四段结构喷管的数值模拟的结果表明，相比不分段而言分段结构可减少一半冷却剂流量。
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