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\newcommand{\AI}{\hbox{ARIES-I}}
\newcommand{\AII}{\hbox{ARIES-II}}
\newcommand{\AIII}{\hbox{ARIES-III}}
\newcommand{\TI}{\hbox{TITAN-I}}
\newcommand{\TII}{\hbox{TITAN-II}}
\newcommand{\VTS}{\hbox{V-3Ti-1Si}}
\newcommand{\VCT}{\hbox{V-15Cr-5Ti}}
\newcommand{\HT}{\hbox{HT-9}}
\newcommand{\degC}{$^\circ$C}
\newcommand{\SdegC}{$\,^\circ$C}
\newcommand{\SPL}{MgAl$_2$O$_4$}
\newcommand{\AlO}{Al$_2$O$_3$}
\newcommand{\LNO}{LiNO$_3$}
\newcommand{\Z}{\phantom{0}}
\newcommand{\D}{\phantom{.0}}
\newcommand{\Y}{\phantom{$\sim$ }}
\newcommand{\X}{\times}
\newcommand{\Dtf}{\hbox{$\Delta T_f$}}
\newcommand{\Dtw}{\hbox{$\Delta T_w$}}
\newcommand{\WR}{\hbox{W-26Re}}
\newcommand{\LZ}{Li$_2$ZrO$_3$}
\newcommand{\LS}{Li$_4$SiO$_4$}
\newcommand{\LO}{Li$_2$O}
\newcommand{\blank}{$\underline{\qquad\qquad\qquad}$}

\title{\bf 10.~~ARIES-I SAFETY DESIGN AND ANALYSIS}
\author{
\hbox to \hsize{
\hbox to 2.truein{      J.~Stephen Herring \hfil}\hfil
\hbox to 2.truein{\hfil Edward T.~Cheng    \hfil}\hfil
\hbox to 2.truein{\hfil Steven P.~Grotz    }}\\ 
\hbox to \hsize{
\hbox to 2.truein{      Shu-Kay Ho         \hfil}\hfil
\hbox to 2.truein{\hfil Kenneth R.~Schultz \hfil}\hfil
\hbox to 2.truein{\hfil Dai-Kai Sze        }}\\ 
\hbox to \hsize{
\hbox to 2.truein{                         \hfil}\hfil
\hbox to 2.truein{\hfil Clement P.~C.~Wong \hfil}\hfil
\hbox to 2.truein{\hfil                    }}\\
}
\date{ }
\maketitle
\begin{titlepage}
{%\baselineskip=1.8ex
\tableofcontents
}
\end{titlepage}

\setcounter{page}{1}
\setcounter{chapter}{9}

\chapter{ARIES-I SAFETY DESIGN AND ANALYSIS}

\section{INTRODUCTION}
\label{s-10-1}

Safety---of the general public, of the operators, and of the investors in a
fusion power plant---has been of paramount importance in the \AI\ design
effort. The \AI\ design team has made low radioactive inventories and the
avoidance of toxic materials central to the reactor design. For this reason, 
silicon-carbide composite is used as the structural material for the blanket 
and divertor as well as for the shield. Helium, which is chemically inert and
is not neutronically activated, is used as the coolant. The zirconium in the 
lithium-zirconate breeder and the tungsten coating on the divertor have been
isotopically tailored to reduce, though certainly not eliminate, the production
of radioactive materials. This section will first review the safety goals for
the \AI\ reactor design (\hbox{Sec.~\ref{s-10-2}}), and then identify the
energy sources that could contribute to an accidental release of hazardous
materials (\hbox{Sec.~\ref{s-10-3}}). The off-site doses resulting from
releases of activation products and of tritium are presented in
\hbox{Sec.~\ref{s-10-4}}. The waste disposal ratings of the reactor materials
are calculated in \hbox{Sec.~\ref{s-10-5}}.  \hbox{Section~\ref{s-10-6}}
discusses the economic benefits of using low-activation materials and the
avoidance of nuclear-grade equipment.  Summary and conclusions are given in
\hbox{Sec.~\ref{s-10-7}}.

\section{SAFETY GOALS IN THE \AI\ DESIGN}
\label{s-10-2}

In order to protect the public from accidents at the reactor, the goal in the
design has been to achieve Level~1 or 2 of safety assurance, as adopted by 
Piet~\cite{Pie86} and the ESECOM study~\cite{Hol89}. A reactor that has
Level~1 safety is ``inherently safe,'' that is, the inventories of radioactive 
materials and stored energy are insufficient to cause prompt fatalities among
the general public at the site boundary. Other authors have defined inherent
safety solely in terms of the inventories of radioactive materials, without
considering whether energy sources are available to release those inventories. 
This section will consider both radioactive inventories and energy sources in
defining inherent safety. A reactor that has Level~2 safety is ``passively
safe,'' that is, it requires no active safety systems to protect the general
public as long as the large-scale passive features of the plant are maintained.

A second safety goal is to maintain inventories of radioactive and toxic
materials in the plant low enough so that an off-site evacuation plan is
unnecessary. A third goal for protecting the public in the long term is that
all wastes produced by the plant be disposable as Class~C waste in shallow land
burial as regulated by 10CFR61~\cite{CFR61}.

Investor safety is enhanced by using factory fabrication of large components
and extensive testing whenever possible, by keeping the construction time
short, and by achieving a level of public safety such that the viability of the
utility would not be threatened by any event within the plant.

\section{ACCIDENT ANALYSES}
\label{s-10-3}

Two ingredients are necessary for an accident involving radioactive or toxic
materials to endanger the public: (1)~an inventory of a hazardous substance and
(2)~an energy source sufficient to release that substance. The amount of energy
available in the accident determines the maximum temperature reached by the
radioactive material and, thus, the release fraction. The product of release
fraction and the radioactive inventory determine the dose to the general
public.

In the \AI\ design, radioactive inventories have been reduced by choosing
low-activation materials such as silicon carbide and beryllium, and by
isotopically tailoring zirconium and tungsten to reduce easily activated
isotopes. Energy sources have been reduced by using a chemically inert coolant,
by using low-afterheat material (SiC), by isotopically tailoring materials to
reduce afterheat, and by arranging the magnets to prevent a transfer of energy
to more radioactive components.

The two principal energy sources that could cause the accidental release of
hazardous inventories are the afterheat in the breeder and structural materials
(which could cause overheating in case of a loss-of-coolant accident), and the
energy stored in the toroidal-field (TF) magnets.

\subsection{Afterheat}
\label{s-10-3-1}

The induced radioactivities in the structural silicon-carbide (SiC) composite 
and breeder materials (although relatively small compared to metals)  are the
main sources of afterheat for the blanket component. Most of the afterheat in
the SiC composite is due to Si. The major induced radioisotopes from Si that
are contributing to the afterheat are $^{28}$A$\ell$ (half-life 2.24~min),
$^{29}$A$\ell$ (6.56~min), $^{27}$Mg (9.46~min), $^{24}$Na (15~h), $^{28}$Mg
(20.9~h), and $^{31}$Si (2.62~h). These radioisotopes are significant for both
beta and gamma-ray energies. The major induced radioisotopes from carbon,
however, are $^{13}$B (17.4~ms), $^6$He (807~ms), and $^{12}$B (20.2~ms),
indicating the insignificant contribution made by these very short half-life
radioisotopes to the afterheat.

Induced afterheat in the breeder, \LZ, is primarily due to the element Zr. 
Lithium and oxygen produce little afterheat because of the very short 
half-life of induced radioisotopes.  Isotopically-tailored zirconium is used
for the \LZ\ breeder in order to retain the  low-activation characteristics of
the \AI\ blanket. The zirconium is tailored to contain 99.9\% $^{92}$Zr and, 
thus, only 0.1\%  (compared to their 72\% natural abundance) of the high
afterheat isotopes $^{90}$Zr, $^{94}$Zr, and $^{96}$Zr.  Such tailored-Zr
element will produce induced afterheat levels a factor of 6.7 lower than the
natural Zr. The major induced radioisotopes from the tailored \LZ\ breeder that
are contributing to the afterheat are $^{90}$Y (64.1~h), $^{91}$Y (58.5~d),
$^{92}$Y   (3.54~h), $^{89}$Zr (78.4~h), $^{89}$Sr (50.6~d), and $^{95}$Zr
(64.0~d) for  beta decay energy, and $^{89}$Zr, $^{95}$Zr, $^{89*}$Zr
(4.18~min), $^{91*}$Y (49.7~min), $^{90*}$Y (3.19~h), and $^{95}$Nb (35.0~d)
for gamma-ray energy.

The beta decay energies are considered to be deposited at the site of the
decay. However, the gamma-ray energies will be transported and deposited
throughout the materials in the reactor components. The combined beta and
gamma-ray energies deposited in the \AI\ reactor were estimated after four full
power years (FPY) of operation at 5~MW/m$^2$ neutron wall loading. The
afterheat and neutron activation in the \AI\ reactor components was estimated
using the ANISN neutron-transport code~\cite{Eng67} and the REAC*2 
activation-analysis  code~\cite{Man82}. The results are given in
\hbox{Figs.~\ref{f-10-3-1}} for the \AI\ first wall and blanket.

\begin{figure}[p]
\vspace{7.5in}
\caption[Fig-10-3-1]
{Afterheat in the \AI\ (A)~first wall and (B)~blanket breeding zone as
functions of time after shutdown (after 4~FPY at 5-MW/m$^2$ wall loading).}
\label{f-10-3-1}
\end{figure}

Figure~\ref{f-10-3-1}(A) shows the afterheat level at the \AI\ first wall as a
function of time after shutdown. Beta decay energies constitute the primary
afterheat source for the first wall from shutdown to about one hour after
shutdown. Thereafter, until about two days after shutdown, beta and gamma-ray
energies contribute equally to the afterheat. After two days, the first-wall
afterheat is principally due to gamma-rays from the \LZ\ breeder
in the breeding zone. At shutdown, the afterheat level is about 0.4~MW/m$^3$. At
one hour after shutdown, the afterheat level at the first wall drops to
about 0.004~MW/m$^3$, a factor of 100 reduction compared to that at shutdown.
After two days the level of heating drops to three orders of magnitude less
than at shutdown. \hbox{Figure~\ref{f-10-3-1}(B)} shows the afterheat level at
the \AI\ blanket breeding zone.

Figure~\ref{f-10-3-2} gives the afterheat in the \AI\ blanket and shield. The
maximum heating rate is shown to be immediately behind the first wall. The
heating rate is dominated by the decay energies resulting from SiC for only the
first 10~minutes after shutdown. At one hour after shutdown and  thereafter,
the heating rate will be primarily the result of decay energies from the \LZ\
breeder. At shutdown the heating rate is about 0.25~MW/m$^3$, and drops to
about 0.03~MW/m$^3$ after 10~minutes. At one hour after shutdown and
thereafter, the heating level is maintaining at about 0.005~MW/m$^3$.

\begin{figure}[tb]
\vspace*{3.0in}
\caption[Fig-10-3-2]
{Afterheat in the \AI\ blanket and shield  as a function of distance from first
wall (after 4~FPY at 5-MW/m$^2$ wall loading).}
\label{f-10-3-2}
\end{figure}        

\subsection{Loss-of-Coolant Analysis}
\label{s-10-3-2}
      
Selecting materials that generate low levels of afterheat is expected to result
in a blanket design that should suffer few adverse consequences from a
loss-of-coolant accident (LOCA). To verify this assumption, a two-dimensional
(2-D) finite-element model of the \AI\ first wall, blanket, and shield was
prepared and analyzed using the computer code, TOPAZ~\cite{Sha84}. The level of
afterheat in the first wall is quite low, initially 0.4~MW/m$^3$, at the onset
of the LOCA. The afterheat levels throughout the blanket drop by about an order
of magnitude after five minutes.  The following assumptions are made:

\begin{enumerate}
\item{} At the onset of the LOCA, the plasma is quenched instantly.
\item{} The heat removal capacity of the coolant is neglected as the gas
pressure drops.
\item{} All of the structure is initially at a uniform temperature of
700\SdegC.
\item{} The vacuum boundary remains intact and no conduction through it is
provided.
\end{enumerate}

The results of this analysis show that the peak temperature during the LOCA
occurs in the first wall at about 280~seconds into the event. The peak
temperature is 780\SdegC. The temperature rise of $\sim$80\SdegC\ is quite
low and is primarily due to the large volume and heat capacity of the beryllium
in the blanket.  Of particular interest is the determination of the
maximum plasma quench time as determined by temperature excursions in the \AI\
first wall.

The divertor is the one component of the fusion power core (FPC) that does not
have low levels of afterheat and has also been treated to the LOCA analysis.
The divertor consists of a 2-mm-thick coating of tungsten on a helium-cooled 
substrate of SiC composite tubes. At shutdown, the level of afterheat in the
tungsten is $\sim$5~MW/m$^3$ and is approximately constant for periods in
excess of one hour. The divertor target faces into the plasma chamber and
radiates the power to the first wall. Assuming the first wall reaches the
calculated LOCA temperature of 780\SdegC\ and remains constant, then the peak
temperature reached by the divertor target is conservatively estimated to be
1020\SdegC.

\subsection{Superconducting Magnet Transients}
\label{s-10-3-3}

In general, a large amount of energy is stored in the TF magnets.  Release of
this energy may potentially cause damage to the FPC and result in accidental
release of hazardous inventories. The \AI\ reactor utilizes high-field TF coils
with a peak field of 21~T. Several transient scenarios were studied to
determine their safety implications. The characteristics of the TF coils as
used in the transient analysis are shown in \hbox{Table~\ref{t-10-3-1}}. Each
of the coils has been divided into two windings of 87~turns each. The  TF-coil
set is powered by two power supplies so that the windings in each coil are
powered by two independent supplies. Dump resistors and circuit breakers are
located between each of the windings. 

\begin{table}[p]
\caption{}
\centering
{\bf ARIES-I Toroidal-Field Coils$^{\bf (a)}$}
\vspace{1.cm}
\renewcommand{\arraystretch}{1.0}
\begin{tabular}{l @{\hspace{2.truecm}} r}
\hline \\
Number of coils                    &  16 \\
Turns per coil                     & 174 \\
Conductor current (kA)             & 126 \\
Maximum field at the conductor (T) &  21 \\
Stored energy (GJ)                 & 130 \\
Dump resistors (m$\Omega$/winding) &   5 \\
Coupling coefficient between adjacent coils & 0.90 \\
\\ \hline
\multicolumn{2}{l}{$^{(a)}$With internally cooled, conduit conductors.}
\end{tabular}
\label{t-10-3-1}
\end{table}

\begin{table}[p]
\caption{}
\centering
{\bf Toroidal-Field-Magnet Transients Considered}
\vspace{1.0cm}
\hbox to \hsize{\hrulefill}
\begin{enumerate}
\item Routine discharge to establish baseline;
\item Turn-to-turn voltages in adjacent windings due to 10-s delay in opening
by one circuit breaker;
\item Turn-to-turn voltages due to complete failure of single circuit breaker;
\item A 10-$\mu\Omega$ short between adjacent windings, with
10-s delay in opening by one breaker;
\item Arcs of 20~V and 35~V between adjacent windings with
10-s delay in breaker opening;
\item Arcs of 20~V and 35~V between adjacent windings with
complete failure of one breaker;
\item Arcs of 20~V and 35~V within one winding, normal breaker operation.
\end{enumerate}
\hbox to \hsize {\hrulefill}
\label{t-10-3-2}
\end{table}

The safety analysis, using MSCAP~\cite{Msc}, considered a variety of faults, as
shown in \hbox{Table~\ref{t-10-3-2}}. In the  analysis, the coils containing
the fault and its immediately adjacent coils (and their associated resistors
and circuit breakers) were individually modeled, while the remaining 13 coils
were combined into two sets of components. The worst case for arcing, shorts,
and winding-to-winding voltages occurs when those faults are adjacent to the
power supplies.

\clearpage

The most severe of the transients, in terms of energy deposited, are the arcs
within one winding. A model of the quench propagation was developed and used to
account for the partitioning of energy between the arc and the resistive
heating of the copper stabilizer. This model assumes that a quench is initiated
by overcurrent in the winding in which the arc is occurring. The rest of the
coil set continues to discharge routinely through the dump resistors. Quench
fronts begin to propagate in both directions along each turn of the conductor,
beginning from the location of maximum field.  The heat deposition in the
copper stabilizer was modeled, thus partitioning the energy  between the arc
and the stabilizer. The temperature-dependence of copper resistivity and
specific heat were included. The results of this transient showed that the
maximum arc power was 1.2~MW, the total deposited arc energy was 17~MJ, the
maximum quench power ({\it i.e.,} resistive heating of the stabilizer) was
90~MW, and the total deposited quench energy was 2~GJ which is not sufficient
to raise the temperature of a TF magnet to room temperature.

These analyses have shown that a severe magnet transient would not lead to a
release of radioactive material and  the afterheat is the dominant energy
source in terms of radioactive releases. Severe magnet transients, however, have
potential economic consequences because of the plant downtime for repair.

\section{RELEASABLE INVENTORIES AND PUBLIC DOSE}
\label{s-10-4}

In determining the dose to the general public, the analysis must first
establish the radioactive inventories and then estimate release fractions based
on the postulated accident and the energy available to promote that release.
Finally, the transport and deposition of the various radionuclides from the
release point to the person at the site boundary have to be calculated. The
hazard inventories were calculated using the ANISN neutron-transport
code~\cite{Eng67} coupled to the REAC*2 activation-analysis code~\cite{Man82}.
Estimates were made of the  maximum-possible release fractions, and the public
dose was calculated using the FUSECRAC code~\cite{Fus}. The worst case weather
conditions used in calculating off-site doses~\cite{Por89} following accidental
release of tritium, zirconium, or tungsten are shown in
\hbox{Table~\ref{t-10-4-1}}. Radioactive inventories, release fractions, and
the resulting public doses are described in this section for the various
radioactive reactor components.

\begin{table}[t]
\caption{}
\centering
{\bf Worst-Case Weather Conditions\\
Used in the FUSECRAC Code$^{\bf (a)}$}
\vspace{0.5cm}
\renewcommand{\arraystretch}{1.3}
\begin{tabular}{l @{\hspace{1.5truein}} c}
\hline \\
Stability                   &  Class F \\
Windspeed (m/s)             &    1 \\
Inversion layer height (m)  &  250 \\
Population density (km$^2$) &   50 \\
Plume dimensions (m)\\
\quad $\sigma_y$            &  100 \\
\quad $\sigma_z$            & \Z50 \\
Puff release duration (min) & 3 \\
Deposition velocity (m/s)   & 0.01 \\
\\ \hline
\multicolumn{2}{l}{$^{(a)}$Ground level release.}
\end{tabular}
\label{t-10-4-1}
\end{table}

\subsection{Lithium-Zirconate Breeding Material}
\label{s-10-4-1}

During the scoping phase of the \AI\ study, three tritium breeders were
considered for use in the \AI\ design: \LS, \LZ, and \LO. Initial analyses
focused on the \LS\ because of its low activation and low afterheat.
Lithium-zirconate, however, was selected as the reference solid breeder because
the data base demonstrates long-term and high-temperature stability.
Unfortunately, the use of zirconium poses much more severe activation concerns
because of the production of $^{89}$Zr (half-life  78.4~h), resulting in high
doses due to accidental releases and because of the production of $^{93}$Zr
(1.5~My), a concern in radioactive waste management. Extensive isotopic
tailoring of zirconium would be necessary to reduce the level of decay heat and
improve the waste disposal rating of the blanket.  Laser isotope
separation~\cite{Alv} is the only feasible technique for this tailoring since
both light and heavy isotopes are to be removed. \hbox{Table~\ref{t-10-4-2}}
summarizes the reduction in the off-site dose for several level of enrichment
(tailoring) and the associated costs.

\begin{table}[tb]
\caption{}
\centering
{\bf Off-Site Dose,$^{\bf (a)}$ Waste Disposal Rating, and Cost of\\
Isotopically Tailored Zirconium in ARIES-I}
\vspace{1.cm}
\renewcommand{\arraystretch}{1.2}
\begin{tabular}{l c c c c c c c c}
\hline
 &  Natural$^{(b)}$ && \multicolumn{6}{c}{Isotopically Tailored}\\
 \cline{2-2} \cline{4-9}
\hfil Case \hfil & 1 && 2 & 3 & 4 & 5 & 6 & 7 \\
\hline \\
Isotopic Composition (\%)\\
\quad $^{90}$Zr&  51.45 && 25.73 &  10.29 & \Z5.15 & \Z2.57 & \Z1.03 & \Z0.057\\
\quad $^{91}$Zr&  11.27 && 25.45 &  33.96 &  36.79 &  38.21 &  39.06 & \Z0.013\\
\quad $^{92}$Zr&  17.17 && 38.77 &  51.73 &  56.05 &  58.21 &  59.51 &  99.908\\
\quad $^{94}$Zr&  17.33 &&\Z8.67 & \Z3.47 & \Z1.73 & \Z0.87 & \Z0.35 & \Z0.019\\
\quad $^{96}$Zr& \Z2.78 &&\Z1.39 & \Z0.56 & \Z0.28 & \Z0.14 & \Z0.06 & \Z0.003\\
1-km dose (rem)&  694.1 &&356.6  & 155.9  & 89.03  & 55.47 & 35.52 & \Z4.55\Z \\
Waste disposal rating
               & \Z7.27 &&\Z3.64 & \Z1.47 & \Z0.74 & \Z0.38 & \Z0.17 &\Z0.05\Z\\
Tailoring cost$^{(c)}$ (\$/kg Zr) 
              &    0\D && 66     &   198  &  296   & 391    & 511    & 2097 \\
\\ \hline
\multicolumn{9}{l}{$^{(a)}$Off-site dose calculated based on
releasing 0.1\% of Zr Inventory.}\\
\multicolumn{9}{l}{$^{(b)}$The dominant isotopes contributing to
the dose for natural Zr are:}\\
\multicolumn{9}{l}{\phantom{$^{(a)}$}$^{89}$Zr (72\%{)} and $^{88}$Y
(15\%), both of which are produced by $^{90}$Zr.}\\
\multicolumn{9}{l}{$^{(b)}$Cost based on \$50/swu (separative work unit).}
\end{tabular}
\label{t-10-4-2}
\end{table}

\begin{table}[p]
\caption{}
\centering
{\bf Off-Site Doses  \\
After Release of 0.1\% of the \LZ\ Inventory\\
Using Natural Zirconium$^{\bf (a)}$}
\vspace{1.0cm}
\renewcommand{\arraystretch}{1.1}
\begin{tabular}{l @{\hspace{1.truein}} c c}
\hline
   & Dose (rem) & Dominant Isotope (\% dose) \\
\hline \\
Prompt dose at 1~km \\
\quad Whole body (WB)              &  \Z669.42 & $^{89}$Zr (72.5) \\
\quad Bone marrow (BM)             &  \Z766.48 & $^{89}$Zr (73.4) \\
\quad Lung                         &   1065.96 & $^{89}$Zr (52.9) \\
\quad Large lower intestine (LLI)  &  \Z662.20 & $^{89}$Zr (63.9) \\
WB early dose\\
\quad \Z1~km                       &  \Z691.25 & $^{89}$Zr (70.8) \\
\quad 10~km                        & \Z\Z47.29 & $^{89}$Zr (70.4) \\
\multicolumn{3}{l}{WB chronic dose at 1~km (chronic plus early)}\\
\quad Inhalation + groundshine     &   2162.58 & $^{88}$Y (43.9) \\
\quad Ingestion                    &   1187.44 & $^{90}$Sr (33.6) \\
\quad Total                        &   3349.48 & $^{88}$Y (32.4) \\
\multicolumn{3}{l}{WB chronic dose at 10~km (chronic plus early)}\\
\quad Inhalation + groundshine     &  \Z148.99 & $^{88}$Y (44.3) \\
\quad Ingestion                    & \Z\Z82.01 & $^{90}$Sr (33.8) \\
\quad Total                        &  \Z230.98 & $^{88}$Y (32.6) \\
Cancers \\
\quad All organs                   &  \Z398.29 & $^{95}$Nb (31.0) \\
\quad WB                           &  \Z133.22 & $^{95}$Nb (26.4) \\
Population dose \\
\quad WB ($\X 10^3$~man-rem)      &   \Z843.98 & $^{95}$Nb (26.4) \\
\\
Waste disposal rating             & \Z\Z\Z0.13 & $^{93}$Zr (66.6) \\
\\ \hline
\multicolumn{3}{l}{$^{(a)}$For 35,420~kg of inventory and
irradiated for 4~FPY at 5~MW/m$^2$.}\\
\multicolumn{3}{l}{\phantom{$^{(a)}$}The initial isotopic composition is:}\\
\multicolumn{3}{l}{\phantom{$^{(a)}$}$^{90}$Zr (51.45\%), $^{91}$Zr 
(11.27\%), $^{92}$Zr  (17.17\%), $^{94}$Zr  (17.33\%), $^{96}$Zr (2.78\%).}
\end{tabular}
\label{t-10-4-3}
\end{table}

\begin{table}[p]
\caption{}
\centering
{\bf Off-Site Doses  \\
After Release of 0.1\% of the \LZ\ Inventory\\
Using Moderately Tailored Zirconium$^{\bf (a)}$}
\vspace{1.0cm}
\renewcommand{\arraystretch}{1.1}
\begin{tabular}{l @{\hspace{1.truein}} c c}
\hline
   & Dose (rem) & Dominant Isotope (\% dose) \\
\hline \\
Prompt dose at 1~km \\
\quad Whole body (WB)             &  \Z34.41 & $^{89}$Zr (80.3) \\
\quad Bone marrow (BM)            &  \Z39.17 & $^{89}$Zr (81.8) \\
\quad Lung                        &   236.30 & $^{91}$Y (75.4) \\
\quad Large lower intestine (LLI) &  \Z63.50 & $^{89}$Zr (37.9) \\
WB early dose\\
\quad \Z1~km                      &  \Z38.35 & $^{89}$Zr (72.7) \\
\quad 10~km                       & \Z\Z2.61 & $^{89}$Zr (72.6) \\
\multicolumn{3}{l}{WB chronic dose at 1~km (chronic plus early)}\\
\quad Inhalation + groundshine    &  \Z99.71 & $^{89}$Y (44.4) \\
\quad Ingestion                   &   308.73 & $^{90}$Sr (49.6) \\
\quad Total                       &   408.38 & $^{90}$Sr (37.6) \\
\noalign{\vskip4pt}
\multicolumn{3}{l}{WB chronic dose at 10~km (chronic plus early)}\\
\quad Inhalation + groundshine    & \Z\Z6.85 & $^{89}$Zr (44.0) \\
\quad Ingestion                   &  \Z21.43 & $^{90}$Sr (49.7) \\
\quad Total                       &  \Z28.27 & $^{90}$Sr (41.3) \\
Cancers \\
\quad All organs                  &  \Z97.26 & $^{91}$Y (47.6) \\
\quad WB                          &  \Z21.07 & $^{90}$Sr (41.3) \\
Population dose \\
\quad WB ($\X 10^3$~man-rem)      &   133.41 & $^{90}$Sr (41.3) \\
\\
Waste disposal rating             & \Z\Z0.03 & $^{93}$Zr (96.4) \\
\\ \hline
\multicolumn{3}{l}{$^{(a)}$For 35,420~kg of inventory and
irradiated for 4~FPY at 5~MW/m$^2$.}\\
\multicolumn{3}{l}{\phantom{$^{(a)}$}The initial isotopic composition is:}\\
\multicolumn{3}{l}{\phantom{$^{(a)}$}$^{90}$Zr (1.03\%), $^{91}$Zr 
(39.06\%), $^{92}$Zr  (59.51\%), $^{94}$Zr  (0.35\%), $^{96}$Zr (0.06\%).}
\end{tabular}
\label{t-10-4-4}
\end{table}

The off-site doses resulting from accidental releases of 0.1\% of the \LZ\
using natural zirconium are shown in \hbox{Table~\ref{t-10-4-3}}. For a
comparison, \hbox{Table~\ref{t-10-4-4}} summarizes the off-site doses using the
tailored zirconium shown as Case~6. In this tailoring, the concentrations of
$^{90}$Zr, $^{94}$Zr, and $^{96}$Zr have been reduced by a factor of 50 from
their natural concentrations. Note that the \hbox{1-km} early dose has been
reduced by about a factor of 20 from the natural zirconium case.

The reference \AI\ breeder is enriched to 99.9\% in $^{92}$Zr at the
considerable cost of $\sim$\$2100/kg (Case 7 of \hbox{Table~\ref{t-10-4-2}}).
Even at this level of enrichment, the total off-site dose of the \AI\ reactor
is still dominated by the Zr.  Other solid breeders such as \LO\ and \LS\ can
be used as alternative solid breeders. These are low-activation breeders that
do not require isotopic tailoring, and their use would drastically reduce the
off-site dose of the \AI\ reactor.

The cases shown in \hbox{Tables~\ref{t-10-4-3}} and \ref{t-10-4-4} assume a
release of 0.1\% of the total zirconium inventory. We have assumed that one of
the 64 blanket modules fails due to overpressure and that two adjacent modules
are damaged by the failure. For solid breeders, which may contain small
particulates due to radiation damage, one can generally assume a release
fraction of 1\%--3\%~\cite{Pie89}. Thus, the release fraction assumed is
\hbox{(3/64) $\X$ 2\%} or approximately 0.1\% of the total zirconium 
inventory. Furthermore, 0.1\% is consistent with a dust release, since  the
afterheat is not sufficient to volatilize the ceramic breeder.

If dust generation is determined to be a severe problem because of radiation
damage, a greater enrichment would be required. As the \AI\ reference case, we
have considered a 2\% release of the entire Zr inventory. This case, as
summarized in  \hbox{Table~\ref{t-10-4-5}}, represents an accident in which all
of the 64 blanket modules fail simultaneously, as they might because of
helium-coolant overpressure.  The zirconium has been very strongly tailored,
such that the concentration of $^{92}$Zr is 99.91\%. The cost of tailoring is
estimated at \$2,097/kg of Zr using ALVIS~\cite{Alv} at \$50/swu.

\begin{table}[p]
\caption{}
\centering
{\bf Off-Site Doses  \\
After Release of 2\% of the \LZ\ Inventory\\
Using Strongly Tailored Zirconium$^{\bf (a)}$ \\
(\AI\ reference case)}
\vspace{1.0cm}
\renewcommand{\arraystretch}{1.05}
\begin{tabular}{l @{\hspace{0.5truecm}} c c}
\hline
   & Dose (rem) & Dominant Isotope (\% dose) \\
\hline \\
Prompt dose at 1 km\\
\quad Whole body (WB)         &  \D\Z63.68 & $^{89}$Zr (57.6) \\
\quad Bone marrow (BM)        &  \D\Z71.05 & $^{89}$Zr (59.9) \\
\quad Lung                    &   1,056.97 & $^{91}$Y (71.3) \\
\quad Large lower intestine (LLI) &  \D319.74 & $^{90}$Y (37.9) \\
WB early dose\\
\quad \Z1~km                  &  \D\Z91.04 & $^{89}$Zr (40.6) \\
\quad 10~km                   & \D\Z\Z6.12 & $^{89}$Zr (41.2) \\
\multicolumn{3}{l}{WB chronic dose at 1~km (chronic plus early)}\\
\quad Inhalation + groundshine &   \D261.63 & $^{88}$Y (53.2) \\
\quad Ingestion               &   2,918.39 & $^{89}$Sr (63.8) \\
\quad Total                   &   3,179.96 & $^{89}$Sr (59.3) \\
\multicolumn{3}{l}{WB chronic dose at 10~km (chronic plus early)}\\
\quad Inhalation + groundshine &  \D\Z17.88 & $^{88}$Y (54.1) \\
\quad Ingestion               &   \D202.74 & $^{89}$Sr (63.7) \\
\quad Total                   &   \D220.61 & $^{89}$Sr (59.3) \\
Cancers\\
\quad All organs              &   \D783.60 & $^{89}$Sr (52.9) \\
\quad WB                      &   \D199.54 & $^{89}$Sr (66.3) \\
Population dose \\
\quad WB ($\X 10^3$ man-rem)  &   1,262.21 & $^{89}$Sr (66.3) \\
\\
Waste disposal rating         & \D\Z\Z0.05 & $^{93}$Zr (99.8) \\
\\ \hline
\multicolumn{3}{l}{$^{(a)}$For 35,420~kg of inventory and
irradiated for 4~FPY at 5~MW/m$^2$.}\\
\multicolumn{3}{l}{\phantom{$^{(a)}$}The initial isotopic composition is:}\\
\multicolumn{3}{l}{\phantom{$^{(a)}$}$^{90}$Zr (0.06\%), $^{91}$Zr 
(0.01\%), $^{92}$Zr  (99.91\%), $^{94}$Zr  (0.02\%), $^{96}$Zr (0.\%).}\\
\multicolumn{3}{l}{\phantom{$^{(a)}$}Note that the off-site dose
is still dominated by $^{89}$Zr.}
\end{tabular}
\label{t-10-4-5}
\end{table}

Although this is fairly extensive isotopic tailoring, the total cost, \$72~M
for the complete reactor, is a small fraction of the total reactor cost. Note
that the release fraction can be limited to 2\% of the total zirconium
inventory because the energy sources available to cause the release ({\it
i.e.,} the decay heat and the compressed helium), are insufficient to drive the
inventory out of the containment. Neither SiC nor the breeder react with the
coolant or air at the temperatures that can be attained in a LOCA. A
determining factor in the transport of the Zr inventory is the size
distribution of the lithium-zirconate particles after the rupture of the
blanket modules. If further data show that the breeder ceramic maintains its
geometric integrity at high fluences ({\it e.g.} ceramic does not disintegrate
into a fine powder), the release fraction from the reactor building could
decrease below the assumed 2\% level, especially since the distance to the site
boundary is 1~km and particles greater than 10~microns would not remain
airborne.

\subsection{Tungsten Coating on the Divertor}
\label{s-10-4-2}

The \AI\ divertor plates are coated with a 2-mm-thick layer of tungsten. The
area of the tungsten coating is 150~m$^2$. That tungsten, and the rhenium
resulting from neutron activation, will be released if the hot surfaces of the
divertor are exposed to air during an accident. In recent experiments at 
INEL~\cite{Smo89}, an inductively heated sample of a  tungsten alloy was
exposed to upward flowing air in a vertical tube. The sample, 10.4~mm in
diameter by 4.7~mm thick, contained the following elements
(concentrations given in wt~\%): W (95\%), Ni (2.3\%), Re (1.1\%), Fe (1.0\%),
Co (0.55\%), Ta (0.15\%), Os (0.06\%), Cu (0.05\%), and Mn (0.05\%).
The measured volatilization rates are given in \hbox{Table~\ref{t-10-4-6}}.

\begin{table}[b]
\caption{}
\centering
{\bf Experimental Tungsten-Alloy Volatilization Rates}
\vspace{1.cm}
\renewcommand{\arraystretch}{1.2}
\begin{tabular}{l @{\hspace{1.cm}} c @{\hspace{1.cm}} c @{\hspace{1.cm}} c}
\hline
 & & \multicolumn{2}{c}{Volatilization Rates (g/h-m$^2$)}\\
 \cline{3-4}
Temperature (\degC) & Duration (h)  & W & Re \\
\hline \\
\Z600 &  20 & $1.4\X 10^{-2}$ & $1.9\X 10^{-2}$ \\
\Z800 & \Z1 &    \Z0.12       &    5.2          \\
      & \Z5 & $6.8\X 10^{-4}$ &    2.4          \\
      &  20 &     \Z0.14      &    1.3          \\
 1000 & \Z1 &       1.2       &   12.4\Z        \\
      & \Z5 & $5.4\X 10^{-2}$ &    4.4          \\
      &  20 &     \Z0.51      &    2.6          \\
 1200 & \Z1 &      36.4\Z     &   11.2\Z        \\
Maximum release & & 0.2\% & 14\% \\
\\ \hline
\end{tabular}
\label{t-10-4-6}
\end{table}

\begin{table}[p]
\caption{}
\centering
{\bf Off-Site Doses  \\
After Accidental Release of Tungsten-Rhenium$^{\bf (a)}$ \\
(ARIES-I reference case)}
\vspace{1.0cm}
\renewcommand{\arraystretch}{1.0}
\begin{tabular}{l @{\hspace{1.truein}} c c}
\hline
   & Dose (rem) & Dominant isotope (\% dose) \\
\hline \\
Prompt dose at 1~km \\
\quad Whole body (WB)             & \Z\Z9.34 & $^{186}$Re (90.2) \\
\quad Bone marrow (BM)            &  \Z13.96 & $^{186}$Re (91.9) \\
\quad Lung                        &   140.71 & $^{186}$Re (98.2) \\
\quad Large lower intestine (LLI) &  \Z26.48 & $^{186}$Re (95.4) \\
WB early dose\\                               
\quad \Z1~km                      &  \Z11.20 & $^{186}$Re (91.2) \\
\quad 10~km                       & \Z\Z0.76 & $^{186}$Re (91.4) \\
\multicolumn{3}{l}{WB chronic dose at 1~km (chronic plus early)}\\
\quad Inhalation + groundshine    &  \Z18.98 & $^{186}$Re (77.1) \\
\quad Ingestion                   &   294.07 & $^{186}$Re (95.1) \\
\quad Total                       &   312.99 & $^{186}$Re (94.0) \\
\multicolumn{3}{l}{WB chronic dose at 10~km (chronic plus early)}\\
\quad Inhalation + groundshine    & \Z\Z1.30 & $^{186}$Re (77.0) \\
\quad Ingestion                   &  \Z20.07 & $^{186}$Re (95.1) \\
\quad Total                       &  \Z21.36 & $^{186}$Re (94.0) \\
Cancers\\
\quad All organs                  &   128.23 & $^{186}$Re (82.8) \\
\quad WB                          &  \Z56.22 & $^{186}$Re (93.6) \\
Population dose \\
\quad WB ($\X 10^3$ man-rem)      &   356.28 & $^{186}$Re (93.6) \\
\\
Waste disposal rating             & \Z\Z0.10 & $^{178*}$Hf (65.0) \\
\\ \hline
\multicolumn{3}{l}{$^{(a)}$For 5,790~kg of inventory and
irradiated for 2~FPY at 1~MW/m$^2$.}\\
\multicolumn{3}{l}{\phantom{$^{(a)}$}Accident duration: 10~h at
1000\SdegC.}\\
\multicolumn{3}{l}{\phantom{$^{(a)}$}Release fractions: 0.0327\% of W
and 29.2\% of Re.}\\
\multicolumn{3}{l}{\phantom{$^{(a)}$}The initial isotopic composition is:}\\
\multicolumn{3}{l}{\phantom{$^{(a)}$}$^{180}$W (0.02\%), $^{182}$W
(3.23\%), $^{183}$W  (90.00\%), $^{184}$W  (3.76\%), $^{185}$W (3.51\%).}
\end{tabular}
\label{t-10-4-7}
\end{table}

In assessing the off-site doses from an air ingress accident on the \AI\ 
reactor, we have assumed the worst-case tungsten release to be a 
\hbox{1273-K}, \hbox{10-h} LOCA in which the \hbox{1-h} release rates are used
for the full 10~hours to account for the flaking off of any protective oxide
resulting from vibration during the accident. The divertor temperature during
the LOCA is based on an analysis in which the plasma is shut off within
15~seconds of the loss of coolant. The off-site doses are shown in
\hbox{Table~\ref{t-10-4-7}}  for the case of tungsten enriched to 90\%
$^{183}$W and irradiated for two full power years (FPY) at 1~MW/m$^2$. The
release fractions of 0.03\% for the tungsten and 29.2\% for the rhenium are
based on the volatilization rates shown in \hbox{Table~\ref{t-10-4-6}}. All
other elements are assumed to be volatized at the detection limit in the
experiment. The off-site doses for other isotopic compositions and other
irradiation times are shown in \hbox{Table~\ref{t-10-4-8}}. 

\begin{table}[p]
\caption{}
\centering
{\bf Off-Site Doses (rem) \\
After Accidental Release of Tungsten-Rhenium$^{\bf (a)}$ \\
(including ARIES-I tungsten-air reaction)}
\vspace{1.0cm}
\renewcommand{\arraystretch}{1.0}
{\small
\begin{tabular}{l @{\hspace{1.truecm}} c c c}
\hline
   & Natural W$^{(b)}$ & 2.86\% $^{186}$W$^{(c)}$ & 90\% $^{183}$W$^{(d)}$ \\
\hline \\
%  & \hbox to 2.truein{\hfil} & \hbox to 1.truein{\hfil}
%   & \hbox to 1.truein{\hfil}  \\
After 0.5~FPY at 1~MW/m$^2$ \\
\quad Early 1~km (rem)      &   \Z8.71    &   \Z3.62    &  \Z1.14 \\
\quad Population dose
($\X 10^3$~man-rem)         &   119.230   &   101,696   & \Z17.496 \\
\quad Waste disposal rating &   \Z0.11    &   \Z0.14    &  \Z0.01 \\
After 1.0~FPY at 1~MW/m$^2$ \\
\quad Early 1~km (rem)      &    24.06    &    16.88    &    3.45 \\
\quad Population dose
($\X 10^3$~man-rem)         &   638.121   &   550.529   & \Z95.376 \\
\quad Waste disposal rating &   \Z0.24    &   \Z0.29    &  \Z0.03 \\
After 2.0~FPY at 1~MW/m$^2$ \\
\quad Early 1~km (rem)      &    57.63    &    46.81    &   11.2\Z \\
\quad Population dose 
($\X 10^3$~man-rem)         & 1,789.443\D & 1,587.206\D &   356.280 \\
\quad Waste disposal rating &   \Z0.57    &   \Z0.65    &   \Z0.10 \\
After 3.0~FPY at 1~MW/m$^2$ \\
\quad Early 1~km (rem)      &    85.57    &    73.15    &    21.61 \\
\quad Population dose
($\X 10^3$~man-rem)         & 2,754.533\D & 2,510.282\D &   704.716 \\
\quad Waste disposal rating &   \Z0.99    &   \Z1.08    &   \Z0.20 \\
After 4.0~FPY at 1~MW/m$^2$ \\
\quad Early 1~km (rem)      &   108.53\Z  &    95.59    &    33.79 \\
\quad Population dose
($\X 10^3$~man-rem)         & 3,558.365\D & 3,296.640\D & 1,110.428\D \\
\quad Waste disposal rating &   \Z1.50    &   \Z1.58    &   \Z0.35 \\
After 5.0~FPY at 1~MW/m$^2$ \\
\quad Early 1~km (rem)      &126.86      &114.72        &    47.1\Z \\
\quad Population dose
($\X 10^3$~man-rem)         &4,198,197   &3,965,330     & 1,552.344\D \\
\quad Waste disposal rating &2.05        &2.13          &   \Z0.54 \\
\\ \hline
\multicolumn{4}{l}{$^{(a)}$For divertor area of 15~m$^2$, tungsten coating
thickness of 2~mm.}\\
\multicolumn{4}{l}{\phantom{$^{(a)}$}Accident duration: 10~h at
1000\SdegC.}\\
\multicolumn{4}{l}{\phantom{$^{(a)}$}Release fractions: 0.0327\% of W
(1.2~g/h-m$^2$) and 29.2\% of Re (12.4~g/h-m$^2$), and}\\
\multicolumn{4}{l}{\phantom{$^{(a)}$}0.20\% of others (0.0114~g/h-m$^2$) using
Ta data.}\\
\multicolumn{4}{l}{$^{(b)}$The initial isotopic composition is:}\\
\multicolumn{4}{l}{\phantom{$^{(b)}$}$^{180}$W (0.13\%), $^{182}$W
(26.30\%), $^{183}$W  (14.30\%), $^{184}$W  (30.67\%), $^{186}$W (28.60\%).}\\
\multicolumn{4}{l}{$^{(c)}$The initial isotopic composition is:}\\
\multicolumn{4}{l}{\phantom{$^{(b)}$}$^{180}$W (0.18\%), $^{182}$W
(35.78\%), $^{183}$W  (19.46\%), $^{184}$W  (41.73\%), $^{186}$W (2.86\%).}\\
\multicolumn{4}{l}{$^{(d)}$The initial isotopic composition is:}\\
\multicolumn{4}{l}{\phantom{$^{(b)}$}$^{180}$W (0.02\%), $^{182}$W
(3.23\%), $^{183}$W  (90.00\%), $^{184}$W  (3.76\%), $^{186}$W (3.51\%).}
\end{tabular}
}
\label{t-10-4-8}
\end{table}

\subsection{Tritium Inventories}
\label{s-10-4-3}

The tritium inventories in the plasma-facing components are calculated by using
the DIFFUSE code~\cite{Bas83}, developed by Sandia National Laboratories. The
DIFFUSE code uses diffusion as the only mechanism for the tritium mass transfer
inside the solid. In the \AI\ design, we investigated the effects of sputtering
on the tritium diffusion mechanism. The sputtering process changes the mass
transfer problem at the first wall into a problem with a moving boundary. If
the sputtering removal rate is much faster than the mass diffusion rate, the
tritium within the deposition layer will be removed by the sputtering process,
together with the structural material, before it has enough time to diffuse
forward.

For the \AI\ first-wall design, the tritium penetration depth is about 2~nm,
and diffusion in the SiC is extremely slow, while the sputtering rate of the
first wall is estimated to be 0.2~mm/y. Therefore, the life of the deposition
depth (2~nm) is only about 100~seconds and the maximum tritium inventory within
the first wall cannot exceed the tritium incident on the first wall during
100~seconds. Therefore, the total tritium inventory is only 6~g, compared to a
few kg predicted without considering sputtering.

The tritium production within the Be is estimated to be  1.15~kg/FPY and the
recoil deposition (implantation of energetic tritons recoiling out of the
adjacent \LZ\ particles into the Be) is 1.4~kg/FPY. Therefore, the total
tritium production and deposition rates in the Be are estimated to be
2.5~kg/FPY.  Recent data (Billone~\cite{Bil88} and recent tests of the ATR
reflector Be~\cite{Bal89}) indicate that the tritium is released from the
beryllium at temperatures above 883~K. Less than one quarter of the beryllium
in the blanket will have a normal operating temperature below 880~K. Thus, the
tritium inventory in Be after 1~FPY is $\sim$0.64~kg. For \AI, it is proposed 
that the entire blanket temperature be raised to above 883~K at least
once per year, thereby driving out the entire tritium inventory. Therefore, the
maximum tritium inventory in Be would be 0.64~kg.

The \AI\ tritium inventories are summarized in \hbox{Table~\ref{t-10-4-9}}.
The total tritium inventory is about 700~g. Releasing the entire tritium
inventory, using Porter's FUSECRAC calculations for approximately
the same conditions, results in an off-site dose of about 7.1~rem.
It should be noted, however, that the tritium inventory in Be is highly
uncertain and can be higher (or lower) by a factor of 3 to 5.

\clearpage

\begin{table}[t]
\caption{}
\centering
{\bf Tritium Inventories in the \AI\ Design}
\vspace{1.cm}
\renewcommand{\arraystretch}{1.3}
\begin{tabular}{l c l}
\hline
                       & Max. Tritium \\
\hfil Components \hfil & Inventory (g)& \hfil Comments \hfil \\
\hline
\\
Fuel cycle\\
\quad Vacuum pumping    & Small & Using ceramic turbomolecular pump\\
\quad Helium separation & Small & Using Pd diffuser\\
\quad Cryogenic distillation & 50 & Only removing H \\
First wall              & \Z6 & Sputtering removes implanted T\\
Divertor plates         &  10 & Using W on SiC\\
Blanket\\
\quad Breeding material & \Z1 & Selection of breeding material and temperature\\
\quad Be                & 640\Z & 1.~Complete tritium release at $>883$~K\\
                        &       & 2.~Blanket is heated to $>883$~K once a year\\
\\
{\bf Total}             & 707\Z \\
\\ \hline
\end{tabular}
\label{t-10-4-9}
\end{table}

\subsection{Silicon-Carbide Structure}
\label{s-10-4-4}

\begin{table}[t]
\caption{}
\centering
{\bf Induced Radioactivities in SiC-Composite First-Wall$^{\bf (a)}$}
\vspace{1.cm}
\renewcommand{\arraystretch}{1.3}
\begin{tabular}{c @{\hspace{1.truecm}} c }
\hline
Time After Shutdown & Activity (Ci/cm$^3$) \\
\hline \\
\phantom{min} \Z1~min & $1.26\X 10^2$\phantom{$^{-}$} \\
\phantom{min} 10~min & $1.31\X 10^1$\phantom{$^{-}$} \\
\phantom{h} \Z1~h   & 1.20 \\
\phantom{h} 10~h   & $6.47\X 10^{-1}$ \\
\phantom{d} \Z1~d   & $3.36\X 10^{-1}$ \\
\phantom{d} 10~d   & $2.31\X 10^{-4}$ \\
\phantom{y} \Z1~y   & $3.60\X 10^{-5}$ \\
\\  \hline 
\multicolumn{2}{l}{$^{(a)}$After 4~FPY of operation at 5~MW/m$^2$.}\\
\end{tabular}
\label{t-10-4-10}
\end{table}

The first wall of the \AI\ blanket is made of SiC-composite structural
material.  \hbox{Table~\ref{t-10-4-10}} gives the induced radioactivities and
associated latent dose ratings resulting from exposure of the SiC composite in
the fusion neutron environment after 4~FPY of operation at 5~MW/m$^2$ wall
loading. The principal contributors to the shutdown activity are $^{28}$A$\ell$
(half-life  2.24~min), $^{24}$Na (15~h), $^{31}$Si (2.6~h), $^{28}$Mg (20.9~h),
and $^{22}$Na (2.2~y), whose decay rates primarily produce the shutdown
radioactivities shown in \hbox{Table~\ref{t-10-4-10}}. The major contributors to
the potential accident dose from the SiC-composite first wall are $^{24}$Na and
$^{22}$Na. 

\subsection{Role of Impurities in Materials}
\label{s-10-4-5}

The impact of impurities in the first wall and shield has been included in the
afterheat analysis in \hbox{Sec.~\ref{s-10-3}}, the dose calculations in
\hbox{Sec.~\ref{s-10-4}}, and the waste disposal evaluation in
\hbox{Sec.~\ref{s-10-5}}. The shield consists of SiC and B$_4$C, while the
first wall is an SiC composite. The impurities in the SiC composite structure
and shield are those assumed in the ESECOM study~\cite{Hol89}. The impurities
in the lithium zirconate were assumed to be the same as those present in
lithium oxide. The impurity concentrations are given in
\hbox{Table~\ref{t-10-4-11}}.

\begin{table}[tb]
\caption{}
\centering
{\bf Impurity Concentration in SiC and \LZ}
\vspace{1.cm}
\renewcommand{\arraystretch}{1.3}
\begin{tabular}{l @{\hspace{3.truecm}} r } \hline
Impurity  & ppm \\
\hline \\
\multicolumn{2}{c}{\us{SiC$^{(a)}$}}\\
 \\
\quad Fe         &    11 \\
\quad Co         &     3 \\
\multicolumn{2}{c}{\us{\LZ$^{(b)}$}}\\
 \\
\quad K          &   370 \\
\quad Ca         &   210 \\
\quad C$\ell$    &   100 \\
\quad Fe         &   100 \\
\quad Pb         &    80 \\
\quad Na         &    50 \\
\quad A$\ell$    &    20 \\
\quad Mn         &    20 \\
\quad Ni         &    20 \\
\quad Si         &    10 \\
\quad Cu         &     5 \\
\\ \hline
\multicolumn{2}{l}{$^{(a)}$From ESECOM study~\cite{Hol89}.}\\
\multicolumn{2}{l}{$^{(b)}$Assumed to be the same as those in \LO.}\\
\end{tabular}
\label{t-10-4-11}
\end{table}

The effect of impurities on afterheat is negligible. Impurities will have
impact on the prompt dose that could be received by the public under worst-case
accident conditions. The dose was estimated by S.~K.\ Ho at the University of
California at Berkeley using the release fractions suggested by
ESECOM~\cite{Hol89} and the FUSEDOSE code~\cite{Fud}. The total prompt dose due
only to impurities could be as high as 21~rem.

\clearpage

\section{WASTE DISPOSAL RATINGS}
\label{s-10-5}

\begin{table}
\caption{}
\centering
{\bf Specific Activity Limits for Class-C Disposal \\
Using 10CFR61 Methodology~\cite{CFR61}}
\vspace{1.cm}
\renewcommand{\arraystretch}{1.0}
\begin{tabular}{l @{\hspace{1.truecm}} c @{\hspace{1.truecm}} c}
\hline
\hfil Radionuclide \hfil & Half-Life (y) & Specific Activity Limit (Ci/m$^3$) \\
\hline \\
\quad $^3$H       & $1.23\X 10^{1}$ & TMSA$^{(a)}$ \\
\quad $^{10}$Be   & $1.60\X 10^{6}$ & 3,000 \\
\quad $^{14}$C    & $5.70\X 10^{3}$ & 700--7,000 \\
\quad $^{26}$Al   & $7.20\X 10^{5}$ & 0.09 \\
\quad $^{32}$Si   & $1.04\X 10^{2}$ & 900--4,000 \\
\quad $^{36}$Cl   & $3.01\X 10^{5}$ & 10--100 \\
\quad $^{39}$Ar   & $2.69\X 10^{2}$ & 10,000 \\
\quad $^{42}$Ar   & $3.30\X 10^{1}$ & 20,000 \\
\quad $^{40}$K    & $1.30\X 10^{9}$ & 1.5 \\
\quad $^{41}$Ca   & $1.03\X 10^{5}$ & 8,000--20,000 \\
\quad $^{44}$Ti   & $4.70\X 10^{1}$ & 200 \\
\quad $^{53}$Mn   & $3.70\X 10^{6}$ & TMSA \\
\quad $^{60}$Fe   & $1.00\X 10^{5}$ & 0.1 \\
\quad $^{60}$Co   & $5.30\X 10^{3}$ & $3\X 10^8$ \\
\quad $^{59}$Ni   & $7.50\X 10^{4}$ & 900 \\
\quad $^{63}$Ni   & $1.00\X 10^{2}$ & $7\X 10^5$--$7\X 10^6$ \\
\quad $^{79}$Se   & $6.50\X 10^{4}$ & 100--1,000 \\
\quad $^{81}$Kr   & $2.10\X 10^{5}$ & 30 \\
\quad $^{85}$Kr   & $1.07\X 10^{1}$ & TMSA \\
\quad $^{87}$Rb
 & \phantom{$^{0}$}$4.80\X 10^{10}$ & TMSA \\
\quad $^{90}$Sr   & $2.85\X 10^{1}$ & $1\X 10^6$--$9\X 10^6$ \\
\quad $^{93}$Zr   & $1.50\X 10^{6}$ & 2,000 \\
\quad $^{91}$Nb   & $6.80\X 10^{2}$ & 200 \\
\quad $^{92}$Nb   & $3.60\X 10^{7}$ & 0.2 \\
\quad $^{93m}$Nb  & $1.36\X 10^{1}$ & TMSA \\
\quad $^{94}$Nb   & $2.00\X 10^{4}$ & 0.2 \\
\end{tabular}
\label{t-10-5-1}
\end{table}


\begin{table}[p]
\centering
{\bf Table 10.5-I. (cont'd)}
\vspace{1.cm}               
\renewcommand{\arraystretch}{1.0}
\begin{tabular}{l @{\hspace{1.truecm}} c @{\hspace{1.truecm}} c}
\hline
\hfil Radionuclide \hfil & Half-Life (y) & Specific Activity Limit (Ci/m$^3$) \\
\hline \\
\quad $^{93}$Mo   & $3.50\X 10^{3}$ & 300 \\
\quad $^{97}$Tc   & $2.60\X 10^{6}$ & 1--10 \\
\quad $^{98}$Tc   & $4.20\X 10^{6}$ & 0.03--0.1 \\
\quad $^{99}$Tc   & $2.13\X 10^{5}$ & 0.2--2 \\
\quad $^{107}$Pd  & $6.50\X 10^{6}$ & TMSA$^{(a)}$ \\
\quad $^{108m}$Ag & $1.27\X 10^{2}$ & 3 \\
\quad $^{113m}$Cd & $1.37\X 10^{1}$ & TMSA \\
\quad $^{121m}$Sn & $5.50\X 10^{1}$ & 10,000 \\
\quad $^{126}$Sn  & $1.00\X 10^{5}$ & 0.1 \\
\quad $^{129}$I   & $1.57\X 10^{7}$ & 30 \\
\quad $^{135}$Cs   & $3.00\X 10^{6}$ & TMSA \\
\quad $^{137}$Cs   & $3.00\X 10^{1}$ & 50,000 \\
\quad $^{133}$Ba   & $1.05\X 10^{1}$ & $2\X 10^8$ \\
\quad $^{137}$La   & $6.00\X 10^{4}$ & 30 \\
\quad $^{138}$La
  & \phantom{$^{1}$}$1.06\X 10^{11}$ & TMSA \\
\quad $^{145}$Pm   & $1.77\X 10^{1}$ & TMSA \\
\quad $^{146}$Pm   & 5.50 & TMSA \\
\quad $^{146}$Sm   & $1.03\X 10^{8}$ & TMSA \\
\quad $^{147}$Sm   
  & \phantom{$^{1}$}$1.06\X 10^{10}$ & TMSA \\
\quad $^{151}$Sm   & $9.00\X 10^{1}$ & TMSA \\
\quad $^{150m}$Eu  & $3.60\X 10^{1}$ & 3,000 \\
\quad $^{152}$Eu   & $1.33\X 10^{1}$ & 300,000 \\
\quad $^{154}$Eu   & 8.80            & $5\X 10^6$ \\
%  & \phantom{.}$8.80$\phantom{$. \X 10^{1}$} & $5\X 10^6$ \\
\quad $^{148}$Gd   & $9.80\X 10^{1}$ & $7\X 10^5$--$7\X 10^6$ \\
\quad $^{150}$Gd   & $1.80\X 10^{6}$ & TMSA \\
\end{tabular}
\end{table}

\begin{table}[p]
\centering
{\bf Table 10.5-I. (cont'd)}
\vspace{1.cm}               
\renewcommand{\arraystretch}{1.0}
\begin{tabular}{l @{\hspace{1.truecm}} c @{\hspace{1.truecm}} c}
\hline
\hfil Radionuclide \hfil & Half-Life (y) & Specific Activity Limit (Ci/m$^3$) \\
\hline \\
\quad $^{157}$Tb   & $1.50\X 10^{2}$ & 1,000 \\
\quad $^{158}$Tb   & $1.50\X 10^{2}$ & 4 \\
\quad $^{154}$Dy   & $2.90\X 10^{6}$ & TMSA$^{(a)}$ \\
\quad $^{166m}$Ho  & $1.20\X 10^{3}$ & 0.2 \\
\quad $^{176}$Lu   
  & \phantom{$^{1}$}$3.59\X 10^{10}$ & TMSA \\
\quad $^{178m2}$Hf & $3.10\X 10^{1}$ & 9,000 \\
\quad $^{182}$Hf   & $9.00\X 10^{6}$ & 0.2 \\
\quad $^{186m}$Re  & $2.00\X 10^{5}$ & 9 \\
\quad $^{187}$Re   
  & \phantom{$^{1}$}$4.00\X 10^{10}$ & TMSA \\
\quad $^{194}$Os   & 6.00            & TMSA \\
%  & \phantom{.}$  
\quad $^{192m2}$Ir & $2.41\X 10^{5}$ & 2 \\
\quad $^{190}$Pt   
  & \phantom{$^{1}$}$6.00\X 10^{11}$ & TMSA \\
\quad $^{193}$Pt   & $5.00\X 10^{1}$ & $9\X 10^6$ \\
\quad $^{194}$Hg   & $5.20\X 10^{2}$ & 0.5 \\
\quad $^{202}$Pb   & $5.30\X 10^{4}$ & 0.6 \\
\quad $^{205}$Pb   & $1.90\X 10^{7}$ & TMSA \\
\quad $^{210}$Pb   & $2.23\X 10^{1}$ & $9\X 10^6$--$8\X 10^7$ \\
\quad $^{207}$Bi   & $3.22\X 10^{1}$ & 8,000 \\
\quad $^{208}$Bi   & $3.68\X 10^{5}$ & 0.09 \\
\quad $^{210m}$Bi  & $3.00\X 10^{6}$ & 1 \\
\quad $^{210}$Po   & $1.02\X 10^{2}$ & 3,000 \\
\\ \hline
\multicolumn{3}{l}{$^{(a)}$Theoretical maximum specific activity allowed
({\it i.e.,} no limit).}
\end{tabular}
\end{table}

\begin{table}[tb]
\caption{}
\centering
{\bf Waste Disposal Ratings of \AI\ Material}
\vspace{1.cm}
\renewcommand{\arraystretch}{1.4}
\begin{tabular}{l @{\hspace{3.5truecm}} c} \hline
\hfil{Component}\hfil & WDR \\
\hline \\
\LZ\ breeder             &  0.05 \\
Tungsten divertor target &  0.10 \\
Tritium                  &  0\Z\Z \\
SiC first wall           &  0.12 \\
SiC/B$_4$C shield        & $< $0.10\phantom{$< $} \\
\\ \hline
\end{tabular}
\label{t-10-5-2}
\end{table}

The waste disposal rating (WDR) is the ratio of the total weighted
concentration of radionuclides in a material to that allowable for Class~C
waste under federal radioactive waste-disposal regulation 10CFR61 (low-level
waste disposed of by near-surface, shallow-land burial)~\cite{CFR61}. Since
10CFR61 was developed for fission reactors, most of the fusion-specific
isotopes are not explicitly listed. The WDRs for each of the materials used in
\AI\ are based on an extension of the methodology of 10CFR61 to all
radionuclides with \hbox{$Z < 88$} by Fetter, Cheng, and Mann~\cite{Fet88}. 
The specific activity limits developed in that extension are shown in
\hbox{Table~\ref{t-10-5-1}}. The WDR is defined as the sum over all nuclides of
the ratio of the actual activity for each nuclide, $\alpha_i$, to the specific
activity for that nuclide for 10CFR61, Class-C low-level waste disposal,
$\alpha_{i,S}$,
%
\begin{eqnarray}
\label{e-10-5-1}
 \hbox{WDR} & = & \sum_i \:
 \left( \frac{\alpha_i}{\alpha_{i,S}}  \right) \: .
\end{eqnarray}

The WDRs of the various components for the reference \AI\ design are shown in
\hbox{Table~\ref{t-10-5-2}}. The WDR of the SiC-composite first wall is 0.12
after 4~full power years of operation at 5~MW/m$^2$-neutron wall loading.  As
can be seen from \hbox{Table~\ref{t-10-5-2}}, all components of \AI\ can be
disposed of as low-level waste under 10CFR61 regulations at the end of their
full design life. Impurities could also affect the WDR. However, it is not
expected that any of the materials that have very low  waste-disposal limits
({\it e.g.,} Nb, Ag, Tb) will be found in the \AI\ materials.

\section{ECONOMIC IMPACT OF SAFETY ISSUES}
\label{s-10-6}

Nuclear-grade materials are used in certain parts of fission power plants.
Because of the excellent safety features of the \AI\ reactor, we considered
which  components in \AI\ should be designated as nuclear grade. A preliminary
analysis of the applicability of the American Society of Mechanical Engineers
(ASME) Boiler and Pressure Vessel Code,  Section~III, Nuclear Plant Components
(hereafter referred to as the Code), has been completed. The Code provides
requirements for the design of pressure-retaining components used in nuclear
power plants.

Topics covered by the Code include items such as material traceability and
testing; minimum strength requirements and allowable stresses; component
fabrication, installation, examination, and testing; overpressure protection;
and documentation and quality assurance requirements. Applicable components are
designated as Class~I, II, or III, depending on their function and importance,
and experience and regulatory interpretation have provided clear guidance on
this classification. Because the Code was written specifically for fission
reactors, it is not directly applicable to a fusion facility.

For nonreactor nuclear facilities, including tritium and fusion facilities,
U.S.\ regulations contained in Department of Energy (DOE) Order 6430.1A require
consideration of the ASME Code requirements in the design and fabrication of
safety class components. Safety class systems are: (1)~Those whose failure could
produce exposure consequences that would exceed the guidelines for limiting
exposure to the public, which is defined as 5~mSv (500~mrem) effective dose
equivalent from early exposure; and (2)~those required to achieve and maintain
the facility in a safe shutdown condition. The DOE Order only mentions design
of safety class components to Class~II rules. This indicates that design of any
components to the more restrictive Class~I rules would not be required for a
fusion facility. Although it is not specifically spelled out in the DOE Order,
it is assumed that designation of some components to the less restrictive 
Class~III would be acceptable if justified based on risk to the public. Based
on a comparison with fission-reactor component functions and classifications, a
general classification scheme has been developed for \AI. Components will be
designed to the Code requirements for Class~II (1)~if they provide a primary
confinement function for significant quantities of radioactive inventories
whose release would produce an individual public dose over 5~mSv (500~mrem),
(2)~if failure could result in a loss of confinement function of these primary
boundaries, or (3)~if they are required to achieve and maintain a safe shutdown
condition.

Components providing support that is necessary for ensuring proper functioning
of Class~II components ({\it i.e.}, secondary cooling systems, and other
components providing a secondary containment function) could be designated as
Class~III. Special consideration must also be given to other components, such
as the magnet sets, that may not fall under the strict Code definition of a 
nuclear-grade component but that may require application of Code criteria in
order to prevent events that could cause physical damage to Class~II
components.

Based on application of these criteria, the preliminary assignment of various
\AI\ components to nuclear-grade classification is summarized in
\hbox{Table~\ref{t-10-6-1}}. This preliminary assignment is not intended to be a
final or all encompassing effort, but is intended primarily to provide
preliminary guidance and to initiate a dialog on the subject to obtain a
consensus among all participants including regulatory agencies. Refinement of
these categories will continue as fusion designs progress and the safety
implications of various component failures is better understood.

\begin{table}[p]
\caption{}
\centering
{\bf Summary of System Classification Based on\\
Preliminary Interpretation of U.S.\ Regulations\break}
\vspace{1.cm}
\renewcommand{\arraystretch}{1.3}
\begin{tabular}{l c l}
\hline
\hfil System\hfil           & Class & \hfil Comments \hfil \\
\hline \\
Vacuum vessel system          & II \\
Vacuum pumping system         & II \\
First-wall heat-transfer system
                              & II & Portions of the system could be\\
                              &    & downgraded if alternate safety-class\\
                              &    & shutdown-cooling system is provided.\\
Divertor heat-transfer system & II & Portions of the system could be\\
                              &    & downgraded if alternate safety-class\\
                              &    & shutdown-cooling system is provided.\\
Breeder heat-transfer system  & II & Same as above except that blanket-coolant\\
                              &   & radioactive inventories must be addressed.\\
Tritium fueling system        & II & At least one primary or secondary system\\
                              &    & must be Class II.\\
Isotope separation system     & II & At least one primary or secondary system\\
                              &    & must be Class II.\\
Fuel storage system           & II \\
Plasma diagnostics attachments& II & Classification depends on extent of\\
                              &    & isolation from the torus.\\
Tritium cleanup system        & III \\
Secondary cooling systems     & III \\
Magnets                       &   & Magnet systems are not directly covered by\\
                              &    & Code but may require design to Code\\
                              &   & requirements to avoid gross coil movement.\\
\\ \hline
\end{tabular}
\label{t-10-6-1}
\end{table}

Department of Energy Order 6430.1A3 requires the use of Section ~III (Nuclear)
of the ASME Code in nonreactor nuclear facilities, including fusion and tritium
facilities. As the Code was written specifically for fission reactors, it is
not directly applicable to a fusion facility such as \AI\ and the question has
been raised as to the applicability of the Code to a fusion facility. One
important concern in this questioning relates to the cost of a fusion facility.
Looking at overall system costs, savings of up to 60\% could be realized if
N-stamped components were not required. The Nuclear Regulatory Commission
regulations for fission reactors (10CFR100~\cite{CFR100}) imply that ASME
Section~III, Class~I requirements must be met if a component failure could
result in a site boundary dose in excess of 0.25~Sv (25~rem). This is 50 times
less restrictive than the DOE 6430.1A3 limit of 5~mSv, but requires more
restrictive Class~I rules. The relationship between these rules must be
clarified as fusion advances from experiments to power plants.

\clearpage

\section{SUMMARY AND CONCLUSIONS}
\label{s-10-7}

The \AI\ study had three specific safety goals:

\begin{enumerate} \item{}That the design achieve either Level of Safety
Assurance~1  or 2. Level of Safety Assurance~1 indicates that the reactor is
inherently safe, having an insufficient radioactive inventory and energy
source to release that inventory to cause prompt fatalities among the general
public. Level of Safety Assurance~2 indicates that the reactor is ``large-scale
passively safe,'' requiring no active safety systems to protect the general
public as long as the large features of the plant are maintained.

\item{}Maintain low enough inventories of radioactive and toxic materials in 
the plants so that an off-site evacuation plan is unnecessary.

\item{}All wastes produced by the plant must be disposable as Class~C 
waste in shallow land burial as regulated by 10CFR61~\cite{CFR61}.

\end{enumerate}

\begin{table}[b]
\caption{}
\centering
{\bf Summary of ARIES-I Off-Site Doses}
\vspace{1.cm}
\renewcommand{\arraystretch}{1.3}
\begin{tabular}{l c l}
\hline 
\hfil Source \hfil & Dose (rem) & \hfil Comments \hfil\\
\hline \\
Zr                  & 91.\Z & Using 99.91\% $^{92}$Zr, 2\% release \\
W                   & 11.2  & Using 90\% $^{183}$W, 10-h LOCA at 1000\SdegC \\
Tritium$^{(a)}$     & \Z6.4 & FUSECRAC analysis, $qf$~=~1 \\
Impurities$^{(b)}$  & 21.\Z & In SiC, B$_4$C, and \LZ \\
\\
{\bf Total}     & 130.\Z\Z \\
\\ \hline
\multicolumn{3}{l}{$^{(a)}$Based on a maximum tritium inventory in Be of 640~g
(Sec.~\ref{s-10-4}).}\\
\multicolumn{3}{l}{$^{(b)}$Using impurity concentrations from
ESECOM~\cite{Hol89}.}\\
\end{tabular}
\label{t-7-1}
\end{table}

By using isotopic tailoring of the zirconium and tungsten and by keeping the
tritium inventory low, the total \hbox{1-km} early dose is $\sim$130~rem
(\hbox{Table~\ref{t-7-1}}). A dose of 200~rem is the minimum required to cause
a prompt fatality to the most sensitive individual. Thus the design is
passively safe because of its use of 99.91\% $^{92}$Zr in the \LZ\ breeder and
90\% $^{183}$W as the tungsten coating. The doses shown assume that 2\% of the
entire \LZ\ inventory is released from the reactor due to the failure of all 64
modules. No credit is assumed for retention of the ceramic breeder material in
the reactor building. The off-site doses due to an air-ingress accident and
tungsten release are based on experimental data on the volatilization of
tungsten and rhenium at 1000\SdegC\ for 10~hours, using the \hbox{1-h} release
rates to account for the loss of protective oxides. The loss-of-coolant
accident analyses of the divertor assume retention of the divertor geometry and
passive ({\it i.e.,} radiative) cooling paths, which limited the maximum
divertor temperature to 1000\SdegC. Without this passive cooling, the divertor
coating would have reached much higher temperatures and release fractions of
tungsten and rhenium would have been substantially higher. The doses due to
impurities in the first wall, blanket, and shield are based on impurity
concentrations and release fractions assumed in the ESECOM study.

An evacuation plan will probably be necessary, since the off-site dose due to
any of the components in \hbox{Table~\ref{t-7-1}} exceeds the 1 to 5~rem
typically adopted by state and local authorities as a threshold level for
evacuation. The off-site doses could be further reduced by using another
breeder, such as \LS\ or \LO.

\clearpage
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%2
\bibitem{Hol89} J.~P.~Holdren, D.~H.~Berwald, R.~J.~Budnitz, J.~G.~Crocker,
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%3
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%4
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%5
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%6
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%7
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%8
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%9
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%10
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%11
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%12
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%14
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%15
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%16
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%17
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%18
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\end{thebibliography}
\end{document}
