skip to main content
OSTI.GOV title logo U.S. Department of Energy
Office of Scientific and Technical Information

Title: Model of a nuclear thermal test pipe using ATHENA. Master's thesis

Technical Report ·
OSTI ID:5245180

Nuclear thermal propulsion offers significant improvements in rocket engine specific impulse over rockets employing chemical propulsion. The computer code ATHENA (Advanced Thermal Hydraulic Energy Network Analyzer) was used in a parametric analysis of fuelpipe. The fuelpipe is an annular particle bed fuel element of the reactor with radially inward flow of hydrogen through it. The outlet temperature of the hydrogen is parametrically related to key effects, including the effect of reactor power at two different pressure drops, the effect of the power coupling factor of the Annular Core Research Reactor, and the effect of hydrogen flow. Results show that the outlet temperature is linearly related to the reactor power and nonlinearly to the change in pressure drop. The linear relationship at higher temperatures is probably not valid due to dissociation of hydrogen. Once thermal properties of hydrogen become available, the ATHENA model for this study could easily be modified to test this conjecture.

Research Organization:
Air Force Inst. of Tech., Wright-Patterson AFB, OH (United States). School of Engineering
OSTI ID:
5245180
Report Number(s):
AD-A-248111/7/XAB; AFIT/GNE/ENP-92M-2
Resource Relation:
Other Information: Thesis (M.S.)
Country of Publication:
United States
Language:
English

Similar Records

Model of a nuclear thermal test pipe using ATHENA
Thesis/Dissertation · Sun Mar 01 00:00:00 EST 1992 · OSTI ID:5245180

Thermal-hydraulic analysis of an annular fuel element: The Achilles' heel of the particle bed reactor
Conference · Wed Jan 20 00:00:00 EST 1993 · AIP Conference Proceedings (American Institute of Physics); (United States) · OSTI ID:5245180

Thermal hydraulic design analysis of ternary carbide fueled square-lattice honeycomb nuclear rocket engine
Journal Article · Fri Jan 22 00:00:00 EST 1999 · AIP Conference Proceedings · OSTI ID:5245180