Analysis of the Radiator Loss Safety Boundary of a Space Reactor Gas Turbine Cycle with Multiple PCU Modules

Analysis of the Radiator Loss Safety Boundary of a Space Reactor Gas Turbine Cycle with Multiple PCU Modules

The development of space exploration technologies puts higher demand on space power systems. The space reactor gas turbine cycle (SRGTC) has the advantages of compact configuration and small mass and volume and is one of the optimal options for future high-power space power systems. The SRGTC operat...

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Bibliographic Details
Main Authors: Wenkui Ma, Ping Ye, Yue Gao, Yadong Hao, Yi Yao, Xiaoyong Yang
Format: Article
Language:English
Published: MDPI AG 2024-01-01
Series:Energies
Subjects:
space reactor
gas turbine cycle
multiple PCU modules
radiator loss
Online Access:https://www.mdpi.com/1996-1073/17/3/597

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https://www.mdpi.com/1996-1073/17/3/597

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