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1. magnetic confinement - ENEA - Fusione

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3. FUSION TECHNOLOGY 97<br />

3.8 Liquid Metal Technology and<br />

Hydrogen Effects on Materials<br />

lithium carbonate (named LC-RT518). The XRD pattern of the final LC-RT518 was in<br />

accordance with the ASTM JCPDS-831454 standards for monoclinic Li 2 CO 3 .<br />

Table 3.IV - Comparison of <strong>ENEA</strong> lithium<br />

carbonate and CEA carbonate sample<br />

Li 2 CO 3 main CEA <strong>ENEA</strong><br />

characteristics sample LC-RT518<br />

Bed density (g/cm 3 ) 0.56 0.45<br />

True density (g/cm 3 ) 2.07 2.06<br />

evaluated closed por. % 2.1 2.2<br />

Spec. Surface area (m 2 /g) 0.90 0.97<br />

Equival. Spher. Dia. (µm) 3.2 3.0<br />

Some further characterisations<br />

were performed on the final LC-<br />

518 carbonate batch, such as true<br />

density by He picnometry, and<br />

specific surface area by nitrogen<br />

adsorption through the classical<br />

three-point Brunauer-Emitt-Teller<br />

(BET) method. The results,<br />

reported in table 3.IV, were<br />

compared with parallel<br />

measurements on a reference<br />

carbonate sample from CEA.<br />

[3.43] P. Lorenzetto,<br />

Technical specification<br />

for the thermal fatigue<br />

tests of Be protected<br />

EDA mock-ups, EFDA<br />

/00-529, 19-11-2001<br />

Fig. 3.38 -Mockup frame<br />

in EDA-BETA.<br />

Fig. 3.39 - CFC electric<br />

radiative resistor.<br />

3.9 Thermal-Fluidodynamics<br />

3.9.1 Fatigue tests on six mockups of primary first-wall panel<br />

prototype (EFDA Contracts 00/529 and 00/533)<br />

The thermal fatigue testing of the first-wall components, i.e., six primary first-wall<br />

mockups (EDA) and two panels, has been committed to <strong>ENEA</strong> [3.43]. The objective<br />

is to perform thermal fatigue on beryllium armoured first-wall test sections. The<br />

experimental campaigns will be performed at <strong>ENEA</strong> Brasimone at the CEF 1-2<br />

thermal-hydraulic facility. For each test campaign, pairs of mockups or panels, to be<br />

tested in parallel, are assembled inside two special vacuum vessels called EDA-BETA<br />

(fig. 3.38) and THESIS. Special CFC electric radiative resistors (fig. 3.39) placed<br />

between each pair of facing mockups provide heating at a nominal heat flux of 0.8<br />

MW/m 2 with a period of 300 s. During the dwell phase, the fatigue stresses are<br />

magnified by inlet cooling water<br />

temperature from 120 to 20 °C.<br />

During the tests, the thermalhydraulic<br />

parameters (coolant,<br />

heater and material<br />

temperatures, water flow rate<br />

and pressure) are also measured.<br />

In 2001, the EDA-BEDA vacuum<br />

chamber was appropriately<br />

modified to provide the mockup<br />

cooling and the electrical<br />

feedthroughs. Preliminary<br />

testing of the modified EDA-<br />

BETA facility was also<br />

performed. Six mockups were<br />

delivered to <strong>ENEA</strong> Brasimone.<br />

They are armoured with Be<br />

grade S65C tiles with different<br />

dimensions and thickness (5 or<br />

10 mm). The heatsink is made of<br />

DS-Cu (Glidcop-Al25) joined to a<br />

stainless steel (AISI316 L) back<br />

plate, both provided with water<br />

cooling channels. At the end of

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