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Management of Commercially Generated Radioactive Waste - U.S. ...

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6.138<br />

quirements, high costs, and probably increased environmental impacts (see Section 6.1.8.4).<br />

Thus, some form <strong>of</strong> waste separation would be required. For HLW, the option appears to be<br />

feasible, on the basis <strong>of</strong> the much lower number <strong>of</strong> Space Shuttle flights that would be<br />

required (approximately one launch per week to dispose <strong>of</strong> HLW from 5000 MT <strong>of</strong> heavy metal<br />

resulting from operations <strong>of</strong> approximately 170 GWe nuclear capacity). It is also possi-<br />

ble that the space option would be used to rid the Earth <strong>of</strong> smaller quantities <strong>of</strong> radio-<br />

active wastes that pose special hazards for long-term terrestrial disposal. The disposal<br />

<strong>of</strong> selected isotopes would require chemical partitioning, with its high costs and secondary<br />

waste streams. Remotely handled and contact-handled TRU wastes from the recycle options<br />

would require geologic disposal.<br />

<strong>Waste</strong>-System Description<br />

The concept for space disposal <strong>of</strong> nuclear waste described here is the current DOE/NASA<br />

reference concept as relfected by the preferred options in Figure 6.1.22. To place the<br />

space disposal concept into perspective from a total system viewpoint, Figure 6.1.23 shows<br />

the waste management system, emphasizing the location and process flow details <strong>of</strong> the space<br />

disposal alternative within the total system. Two points are apparent from this figure:<br />

(1) chemical processing would definitely be required for space disposal <strong>of</strong> waste, and (2)<br />

the mined geologic repository would be part <strong>of</strong> the total system. The following discussion<br />

briefly summarizes the mission pr<strong>of</strong>ile frm the standpoint <strong>of</strong> waste-type compatability,<br />

prelaunch activities, and orbital operations. Battelle (1980) presented a more detailed<br />

discussion <strong>of</strong> this pr<strong>of</strong>ile and various element definitions and requirements.<br />

Prelaunch Activities. The prelaunch activities would include nuclear waste processing<br />

and payload fabrication, ground transportation <strong>of</strong> waste, on-site payload preparation, and<br />

final staging operations.<br />

Typically, spent fuel rods from domestic power plants would be transported to the waste<br />

processing and payload fabrication site in conventional shipping casks (see Chapter 4). A<br />

high-level waste stream containing fission products and actinides, including several tenths<br />

<strong>of</strong> a percent <strong>of</strong> the original plutonium and uranium, would result from the uranium and pluto-<br />

nium recovery process. This waste would be formed into a "cermet" matrix (Aaron et al.<br />

1979) (an abbreviation for ceramic particles uniformly dispersed within a metallic phase),<br />

which has been shown to have superior properties compared with other potential waste forms<br />

for space disposal (Battelle 1980). The waste would then be fabricated into an unshielded<br />

5000-kg sphere. Within a remote shielded cell, this waste payload would be loaded into a<br />

container, which would be closed be sealed, inspected, decontaminated, and packaged into a<br />

flight-weight gamma radiation shield assembly. During these operations and subsequent<br />

interim storage at the processing site, the waste package would be cooled by an auxiliary<br />

cooling system.

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