Actions for Transient heat pipe investigations for space power systems
Transient heat pipe investigations for space power systems
- Author
- Merrigan, M. A.
- Published
- United States : [publisher not identified], 1985
Springfield, Va.: National Technical Information Service, [approximately 1985] - Physical Description
- microfiche : negative ; 11 x 15 cm
- Additional Creators
- Keddy, E. S. and Sena, J. T.
- Summary
- A 4-meter long, high temperature, high power, molybdenum-lithium heat pipe has been fabricated and tested in transient and steady state operation at temperatures to 1500 K. Maximum power throughput during the tests was approximately 37 kW/cm2 for the 1.4 cm diameter vapor space of the annular wick heat pipe. The evaporator flux density for the tests was 150.0 W/cm2 over a length of 40 cm. Condenser length was approximately 3.0 m with radiant heat rejection from the condenser to a coaxial, water cooled radiation calorimeter. A variable radiation shield, controllable from the outside of the vacuum enclosure, was used to vary the load on the heat pipe during the tests. 1 ref., 9 figs.
- Report Numbers
- DE86000813; LA-UR-85-3341; CONF-8509153-4
- Other Subject(s)
- 21 specific nuclear reactors and associated plants
- 220600 - nuclear reactor technology- research, test & experimental reactors
- Alkali metals
- Elements
- Energy transfer
- Heat pipes
- Heat transfer
- Lithium
- Metals
- Mobile reactors
- Molybdenum
- Nesdps office of nuclear energy space and defense power systems
- Performance testing
- Power density
- Power reactors
- Reactors
- Space power reactors
- Testing
- Transition elements
- Very high temperature
- Collection
- NTIS collection.
- Note
- DOE contract number: W-7405-ENG-36
OSTI Identifier 5041804
Research organization: Los Alamos National Laboratory (LANL), Los Alamos, NM (United States).
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