Public Acceptance of ITER-Tokamak Fusion Power

One of the U.S. Electric Power Research Institute’s criteria for practical fusion power is public acceptance. In this analysis we consider the potential public acceptance of ITER-tokamak fusion power. Because ITER-like reactors are not likely to be commercially ready before mid-century, a forecast of public acceptance is very difficult. We break “the public” down into four entities: 1) Rank and file consumers, 2) Governments [local, state, & federal including regulators], 3) NGOs including environmental groups, and 4) Electric utilities. We assert that ITER-tokamaks will be evaluated in the context of fission power because both are nuclear processes. We observe that ITER-tokamak fusion will present radioactive hazards and be extremely expensive. Three possible futures for fission nuclear mid-century are: 1) full acceptance, 2) middling acceptance, and 3) rejection. If fission power is accepted mid-century, then ITER-tokamak fusion stands the best chance of being publicly acceptable, its largest drawback being very high cost. If fission power is of middling acceptance, then ITER-tokamak fusion might be marginally more acceptable because of its much shorter life radioactive waste. If fission power is unacceptable, then ITER-tokamak fusion acceptance will be very difficult.

Application Prospect of Fission-Powered Spacecraft in Solar System Exploration Missions

Fission power is a promising technology, and it has been proposed for several future space uses. It is being considered for high-power missions whose goal is to explore the solar system and even beyond. Space fission power has made great progress when NASA’s 1 kWe Kilowatt Reactor Using Stirling TechnologY (KRUSTY) prototype completed a full power scale nuclear test in 2018. Its success stimulated a new round of research competition among the major space countries. This article reviews the development of the Kilopower reactor and the KRUSTY system design. It summarizes the current missions that fission reactors are being considered as a power and/or propulsion source. These projects include visiting Jupiter and Saturn systems, Chiron, and Kuiper belt object; Neptune exploration missions; and lunar and Mars surface base missions. These studies suggest that the Fission Electric Propulsion (FEP)/Fission Power System (FPS) is better than the Radioisotope Electric Propulsion (REP)/Radioisotope Power System (RPS) in the aspect of cost for missions with a power level that reaches ~1 kWe, and when the power levels reaches ~8 kWe, it has the advantage of lower mass. For a mission that travels further than ~Saturn, REP with plutonium may not be cost acceptable, leaving FEP the only choice. Surface missions prefer the use of FPS because it satisfies the power level of 10’s kWe, and FPS vastly widens the choice of possible landing location. According to the current situation, we are expecting a flagship-level fission-powered space exploration mission in the next 1-2 decades.

APPLICATION OF TWO STAGE METHOD OF CHARACTERISTICS / SP3 METHODOLOGY TO TRISO-FUELLED LEU SPACE REACTOR IN WIMS 11

In order to minimise the mass of a 1MWe LEU space fission power system design, a rapid neutronics analysis tool is sought. A two-stage deterministic analysis routine has been constructed using a core-plane method of characteristics calculation followed by a full-core SP3 calculation, within the ANSWERS© code WIMS11. This is compared to a faster route that skips the core-plane calculation and also the Monte Carlo code Serpent. Results suggest sufficiently good agreement for the WIMS-based methods to be useful in a full system mass-minimising optimisation routine.