Abstract

According to versatile and long-lasting requirements of deep space missions, space nuclear reactor (SNR) power system is becoming a more suitable choice compared to traditional solar and chemical power systems in large-scale and long-life applications. From NASA’s previous research, the gas-cooled reactor along with closed Brayton cycle (CBC) could achieve optimized weight-power ratio and be more applicable for large power system (100 kWe or MWe level). In this paper, a concept of integrated gas-cooled space nuclear reactor named IGCR-200 is introduced, which is designed based on the TRISO particle fuel and could achieve 200 kWe output combined with highly efficient He/Xe CBC generator. The design requirements include an operation lifetime of at least 10 years in full power mode, maximum fuel temperature < 1600K, negative temperature reactivity feedback, passive decay heat removal, redundancy in reactor control, and sub-criticality during water flooding accidents. It has an outer diameter of 70.0 cm, a height of 66.0 cm (reactor part), a total mass around 1000 kg, total Uranium inventory of 226.8 kg (235U enrichment as 93%), and 1 MW thermal power output. The reactor physics, thermal hydraulics and other required analysis are taken out to show the feasibility and performances of the design.

Highlights

  • The nuclear energy in space has been considered as a good option to provide steady and long-lasting electricity supply, especially in situations when and where the solar option is inadequate, impractical, or nonexistent [1]

  • A concept of integrated gas-cooled space nuclear reactor (SNR) named IGCR-200 is proposed, which is designed based on the TRISO particle fuel and could achieve 200 kWe output power combined with highly efficient He/Xe closed Brayton cycle (CBC) power conversion units (PCUs) [7]

  • The neutronics analyses described are performed using the Monte Carlo code RMC [10][11], and a set of continuous energy cross-section libraries from the ENDF-B VII.1 nuclear data was used in the analyses

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Summary

Introduction

The nuclear energy in space has been considered as a good option to provide steady and long-lasting electricity supply, especially in situations when and where the solar option is inadequate, impractical, or nonexistent [1]. The Institute of Nuclear and New Energy Technology (INET) at Tsinghua University has accumulated a lot of research experiences in TRISO particle fuel, inert gas process and direct Brayton cycle conversion system [6], which are the most important aspects in large-scale gas-cooled SNR design. The reactor has an outer diameter of 70.0 cm, a height of 66.0 cm (core part), a total mass around 1000 kg, total Uranium inventory of 226.8 kg (235U enrichment as 93%), and 1.0 MW thermal power output

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