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Journal ArticleDOI

Design of particle bed reactors for the space nuclear thermal propulsion program

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TLDR
In this article, the Particle Bed Reactor (PBR) was considered for the Space Nuclear Thermal Propulsion (SNTP) Program and several new algorithms were developed for fluid dynamics, heat transfer and transient analysis; and commercial codes were used for the stress analysis.
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This article is published in Progress in Nuclear Energy.The article was published on 1996-01-01. It has received 43 citations till now. The article focuses on the topics: Nuclear reactor & Coolant.

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A review of in-pile fuel safety tests of TRISO fuel forms and future testing opportunities in non-HTGR applications

TL;DR: In this article, the authors identify the need for in-pile testing data to support licensing of tristructural isotropic (TRISO) fuel in light water reactors, microreactors, nuclear thermal propulsion, and salt-cooled reactor applications.
Journal ArticleDOI

Innovative concept for an ultra-small nuclear thermal rocket utilizing a new moderated reactor

TL;DR: The Korea Advanced NUClear Thermal Engine Rocket (KANUTER) as discussed by the authors is a new NTR design of the second design philosophy, which consists of an Extremely High Temperature Gas cooled Reactor (EHTGR) utilizing hydrogen propellant, a propulsion system, and an optional electricity generation system to provide propulsion as well as electricity generation.
Journal ArticleDOI

Radial void fraction correlation for annular packed beds

TL;DR: In this paper, the radial void fraction distributions of equal sized spheres in annular packed beds (APBs) were calculated and a radial void factor correlation was obtained from these distributions that can be incorporated in APB transport models.
Journal ArticleDOI

Preliminary conceptual design of a new moderated reactor utilizing an LEU fuel for space nuclear thermal propulsion

TL;DR: In this paper, a low-enriched uranium fuel (KANUTER-LEU) was used for the nuclear thermal rocket (NTR) propulsion, which is a viable option for human exploration into deep-space because of its high thrust, improved specific impulse, well established technology, bimodal capability, and enhanced mission safety and reliability.
Journal ArticleDOI

High performance nuclear thermal propulsion system for near term exploration missions to 100 A.U. and beyond

TL;DR: In this article, a new ultra light nuclear reactor engine design termed MITEE (MIniature Reac Tor EnginE) is described, achieving a specific impulse of 1000 seconds and a thrust-to-weight of 10.
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