Performance demonstration of a high-power space-reactor heat-pipe design
Performance of a 15.9-mm diam, 2-m long, artery heat pipe has been demonstrated at power levels to 22.6 kW and temperatures to 1500/sup 0/K. The heat pipe employed lithium as a working fluid with distribution wicks and arteries fabricated from 400 mesh Mo-41 wt % Re screen. Molybdenum alloy (TZM) was used for the container. Peak axial power density attained in the testing was 19 kW/cm/sup 2/ at 1465/sup 0/K. The corresponding radial flux density in the evaporator region of the heat pipe was 150 W/cm/sup 2/. The extrapolated limit for the heat pipe at its 1500/sup 0/K design point is 30 kW, corresponding to an axial flux density of 25 kW/cm/sup 2/. Sonic and capillary limits for the design were investigated in the 1100 to 1500/sup 0/K temperature range. Excellent agreement of measured and predicted temperature and power levels was observed.
- Research Organization:
- Los Alamos National Laboratory (LANL), Los Alamos, NM (United States)
- DOE Contract Number:
- W-7405-ENG-36
- OSTI ID:
- 6026275
- Report Number(s):
- LA-UR-83-1330; CONF-830812-19; ON: DE83012688
- Resource Relation:
- Conference: 18. intersociety energy conversion engineering conference, Orlando, FL, USA, 21 Aug 1983; Other Information: Portions are illegible in microfiche products
- Country of Publication:
- United States
- Language:
- English
Similar Records
Development and test of a space-reactor-core heat pipe
Transient performance investigation of a space power system heat pipe
Related Subjects
HEAT PIPES
PERFORMANCE TESTING
SPECIFICATIONS
SPACE POWER REACTORS
POWER RANGE 10-100 KW
MOBILE REACTORS
POWER REACTORS
REACTORS
TESTING
NESDPS Office of Nuclear Energy Space and Defense Power Systems
210600* - Power Reactors
Auxiliary
Mobile Package
& Transportable