Comparing Low Enriched Fuel to Highly Enriched Fuel for use in Nuclear Thermal Propulsion Systems-Reference-Cited by-同舟云学术

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Comparing Low Enriched Fuel to Highly Enriched Fuel for use in Nuclear Thermal Propulsion Systems

Published:2016-07-22 Issue: Volume: Page:
ISSN:
Container-title:52nd AIAA/SAE/ASEE Joint Propulsion Conference
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Author:

Patel Vishal,Eades Micheal,Venneri Paolo,Joyner Claude R.

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2016-4887

Reference12 articles.

1. 1Finseth, J. “Overview of Rover Engine Tests (Final Report),” Tech. Rep. NASA-CR-LD4270, National Aeronautics and Space Administration, 1991.

2. Spark Plasma Sintering of W–UO2 cermets

3. A feasibility study on low-enriched uranium fuel for nuclear thermal rockets – I: Reactivity potential

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1. Corrosion and microstructural characterization of molybdenum cermets following hydrogen exposure up to 2630K;Journal of Nuclear Materials;2023-12

2. Feasibility of Low-Enriched Uranium Fueled Nuclear Thermal Propulsion in the Low-Thrust Region Below 16klbf;Annals of Nuclear Energy;2022-12

3. Subscale maturation of advanced reactor technologies (SMART): A path forward for nuclear thermal propulsion fuel and reactor development;Progress in Nuclear Energy;2022-11

4. Establishing the Feasibility of the Centrifugal Nuclear Thermal Rocket;AIAA Propulsion and Energy 2021 Forum;2021-07-28

5. NTP Design Derivatives and Enhancements for Lunar and Mars Missions;AIAA Propulsion and Energy 2019 Forum;2019-08-16

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