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Transient Approximation of SAFE-100 Heat Pipe OperationEngineers at Los Alamos National Laboratory (LANL) have designed several heat pipe cooled reactor concepts, ranging in power from 15 kWt to 800 kWt, for both surface power systems and nuclear electric propulsion systems. The Safe, Affordable Fission Engine (SAFE) is now being developed in a collaborative effort between LANL and NASA Marshall Space Flight Center (NASA/MSFC). NASA is responsible for fabrication and testing of non-nuclear, electrically heated modules in the Early Flight Fission Test Facility (EFF-TF) at MSFC. In-core heat pipes must be properly thawed as the reactor power starts. Computational models have been developed to assess the expected operation of a specific heat pipe design during start-up, steady state operation, and shutdown. While computationally intensive codes provide complete, detailed analyses of heat pipe thaw, a relatively simple. concise routine can also be applied to approximate the response of a heat pipe to changes in the evaporator heat transfer rate during start-up and power transients (e.g., modification of reactor power level) with reasonably accurate results. This paper describes a simplified model of heat pipe start-up that extends previous work and compares the results to experimental measurements for a SAFE-100 type heat pipe design.
Document ID
20050109882
Acquisition Source
Marshall Space Flight Center
Document Type
Conference Paper
Authors
Bragg-Sitton, Shannon M.
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Reid, Robert S.
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Date Acquired
September 7, 2013
Publication Date
January 1, 2005
Subject Category
Spacecraft Propulsion And Power
Meeting Information
Meeting: STAIF 2005 Conference
Location: Albuquerque, NM
Country: United States
Start Date: February 13, 2005
End Date: February 17, 2005
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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