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Title: Thermal-hydraulic analysis of an annular fuel element: The Achilles' heel of the particle bed reactor

Conference · · AIP Conference Proceedings (American Institute of Physics); (United States)
DOI:https://doi.org/10.1063/1.43047· OSTI ID:5588316
;  [1]
  1. Air Force Institute of Technology, Department of Engineering Physics, AFIT/ENP, Wright-Patterson AFB, OH 45433 (United States)

The low pressure nuclear thermal propulsion (LPNTP) concept offers significant improvements in rocket engine specific impulse over rockets employment chemical propulsion. This study investigated a parametric thermal-hydraulic analysis of an annular fueld element, also referred to as a fuel pipe, using the computer code ATHENA (Advanced Thermal Hydraulic Energy Network Analyzer). The fuelpipe is an annular particle bed fuel element of the reactor with radially inward flow of hydrogen through the element. In this study, the outlet temperature of the hydrogen is parametrically related to key effects, including the reactor power at two different pressure drops, the effect of power coupling for in-core testing, and the effect of hydrogen flow rates. Results show that the temperature is linearly related to the reactor power, but not to pressure drop, and that cross flow inside the fuelpipe occurs at approximately 0.3 percent of the radial flow rates.

OSTI ID:
5588316
Report Number(s):
CONF-930103-; CODEN: APCPCS
Journal Information:
AIP Conference Proceedings (American Institute of Physics); (United States), Vol. 271:3; Conference: 10. symposium on space nuclear power and propulsion, Albuquerque, NM (United States), 10-14 Jan 1993; ISSN 0094-243X
Country of Publication:
United States
Language:
English