@inproceedings{c12c3fd5a6c6427485c964c6cd7ea255,
title = "Conceptual design of a CERMET NTR fission core using multiphysics modeling techniques",
abstract = "An initial pre-concenptual CERMET Nuclear Thermal Propulsion reactor system is investigated within this paper. Reactor configurations are investigated where the fuel consists of 60 vol.\% UO2 and 40 vol.\% W where the UO2 consists of Gd2O3 concentrations of 5 and 10 mol.\%.Gd2O3. The fuel configuration consisting of 5 mol.\% UO2 was found to have a total mass of 2761 kg and a thrust to weight ratio of 4.10 and required a coolant channel surface area to fueled volume ratio of approximately 15.0 in order to keep the centerline temperature below 3000 K. The configuration consisting of 10 mol.\% Gd2O3 required a surface area to volume ratio of approximately 12.2 to cool the reactor to a peak temperature of 3000 K and had a total mass of 3200 kg and a thrust to weight ratio of 3.54. It is not known yet what concentration of Gd2O3 is required to maintain fuel stability at 3000 K; however, both reactors offer the potential for operations at 25,000 lb∫ and and at a specific impulse which may range from 900 to 950 seconds.",
author = "Webb, \{Jonathan A.\} and Gross, \{Brian J.\} and Taitano, \{William T.\}",
year = "2011",
doi = "10.2514/6.2011-5947",
language = "English",
isbn = "9781600869495",
series = "47th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit 2011",
publisher = "American Institute of Aeronautics and Astronautics Inc.",
booktitle = "47th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit 2011",
note = "47th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit 2011 ; Conference date: 31-07-2011 Through 03-08-2011",
}