Actions for Request for Design of a Fuel Element Assembly Soak Test [electronic resource].
Request for Design of a Fuel Element Assembly Soak Test [electronic resource].
- Published
- Washington, D.C. : United States. Dept. of Energy, 1961.
Oak Ridge, Tenn. : Distributed by the Office of Scientific and Technical Information, U.S. Dept. of Energy. - Additional Creators
- United States. Department of Energy and United States. Department of Energy. Office of Scientific and Technical Information
Access Online
- Restrictions on Access
- Free-to-read Unrestricted online access
- Summary
- It is requested that the design be completed for a full-scale fuel element soak test. The test assembly must be designed to permit the fuel element test specimen to be submerged in a lithium bath under a pressure of 60 psi. The maximum temperature of the lithium is to be 2000 F. A total of four test units will be required to complete the test program. Two specimens will be exposed to a thermal cycle between 2000 F and 1400 F with the remaining two specimens being exposed to a thermal cycle between 2000 F and 1000 F. Heating will be done at the rate of 200 F/hour preceded by a 150 hour soak at 2000 F. Heat will be supplied by clam-shell type heaters. The test specimen - lithium system will be contained by a Cb-lZr vessel which will be surrounded by a 310 steel container. The heating units will be mounted on the outside of this 310 S.S. container. A bottom fill line is requested in order to insure a lithium system free from gas pockets. A slow lithium fill will be made up through the specimen to a level indicated by a probe in the expansion tank.
- Report Numbers
- E 1.99:cnlm-3911
cnlm-3911 - Subject(s)
- Other Subject(s)
- Note
- Published through SciTech Connect.
11/30/1961.
"cnlm-3911"
Spahl, R.J.
PW (Pratt and Whitney Aircraft (United States)) - Funding Information
- AT(30-1)-2789
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