General Atomics recently completed a divertor design study for JAERI for th
e JT-60 Super Upgrade (JT-60SU) tokamak. JT-60SU is being designed as a sup
erconducting device for an integrated R&D investigation of steady-state ope
ration in a tokamak. A divertor design was developed to accommodate double-
null operation for a 1000 s discharge duration at 8 MA of plasma current an
d 80 MW of auxiliary heating. The work reported here is an extension of a p
revious design study.(1,2) The thermal requirements are a peak heat flux of
9 MW/m(2), a maximum surface temperature of 1600 degreesC, and a poloidal
cooling flow configuration for the plasma facing components. The structural
requirements are determined from both the predicted stresses due to halo c
urrents as well as the stresses due to differential thermal expansion encou
ntered during bakeout. The halo current loads are based on a nominal halo c
urrent of 0.19 Ip with a 2.0 toroidal peaking factor. Analysis has determin
ed that the halo current load per centimeter of circumference is P = 2856 (
1+cos theta) N/cm, where 8 is the toroidal angle. The loads due to differen
tial thermal expansion are a result of an expected 100 degreesC temperature
difference between the vacuum vessel and divertor during bakeout.
Based on the aforementioned criteria, a divertor design was developed for a
ll three areas of the JT-60SU divertor: the inner baffle, the private flux
baffle, and the outer baffle. In order to have highly reliable divertor com
ponents, flexible supports sized to accommodate the structural loads are ut
ilized in the design rather than insulators or sliding interfaces. The plas
ma facing components are mounted on a structural mounting plate to form a r
emovable and remotely-maintainable segment which is in turn mounted on the
supports. For outer and private flux baffles, these structural mounting pla
tes are joined together using a double shear joint design to form a structu
rally continuous ring to react the halo current loads. The plasma facing co
mponents are broken into 80 segmentation; however, the outer and private fl
ux baffles have an alternating 8 degrees and 16 degrees structural segmenta
tion which forms the double shear toroidal structural joint. The inner baff
le takes advantage of its relatively short poloidal length and its proximit
y to the vacuum vessel to provide structural integrity. The thermal design
consists of a plasma facing material of flat CFC tiles that are brazed onto
a poloidally cooled copper heat sink. Adequate gaps between the baffles an
d wall are provided for pumping of recycled gas.