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6.153<br />

* "Treaty on Principles Governing the Activities <strong>of</strong> States in the Exploration and Use <strong>of</strong><br />

Outer Space Including the Moon and Other Celestial Bodies" (1967)<br />

* "Convention on International Liability for Damage Caused by Space Objects" (1972)<br />

* "Agreement on the Rescue <strong>of</strong> Astronauts, the Return <strong>of</strong> Astronauts, and the Return <strong>of</strong><br />

Objects Launched into Outer Space" (1972)<br />

* "Convention on Damage Caused by Foreign Aircraft to Third Parties on the Surface"<br />

(1952)<br />

* "Convention on Registration <strong>of</strong> Objects Launched into Outer Space" (1976).<br />

This list suggests various issues that would have to be thoroughly explored in this early<br />

decision-making phase, including: (1) accident liability, (2) exclusive use <strong>of</strong> the lunar<br />

surface or other regions <strong>of</strong> outer space, and (3) international program involvement (e.g., use<br />

<strong>of</strong> the sea). These issues relate mainly to accident situations rather than routine<br />

operations.<br />

In addition to these political and international issues, space disposal <strong>of</strong> nuclear waste<br />

would have a number <strong>of</strong> legal complexities associated with it, including liability and regula-<br />

tory requirements (e.g., licensing). These concerns would be quite evident not only during,<br />

but also before and after actual implementation. Moreover, legal concerns could lengthen the<br />

time needed to implement a space disposal option.<br />

6.1.8.5 Potential Impacts Over Long Term (Postemplacement)<br />

Postemplacement for the space option is defined as the period <strong>of</strong> time after achievement<br />

<strong>of</strong> a stable solar orbit. Potential impacts during this period are analyzed for two different<br />

events: engineering failure and inadvertent human intrusion.<br />

Potential Events<br />

The possibility <strong>of</strong> sudden failure <strong>of</strong> a container in solar orbit would be extremely remote.<br />

However, if a container should rupture, for example, as a result <strong>of</strong> a meteor impact or<br />

degradation over the long term, the contents would be released and begin to spread. The<br />

physical processes by which the nuclear waste material would be dispersed in solar space<br />

include sputtering, thermal diffusion, and interactions with solar radiation and wind. Large<br />

pieces or particles <strong>of</strong> waste material would be sputtered into smaller particles, which in<br />

turn would disperse. The smallest particles, with radii less than 10- 5 to 10-4 cm, would<br />

be swept out <strong>of</strong> the solar system by direct solar radiation pressure. Larger particles, those<br />

with radii up to 10-3 to 10-2 cm, would gradually loose momentum through scattering,<br />

charge exchange interactions, and collisions with energetic photons and solar wind protons.<br />

This process, called the Poynting Robertson effect, would cause these particles to begin mov-<br />

ing in toward the sun where they would eventually be vaporized and broken down into smaller<br />

particles. Once this had occurred, the smaller particles would be swept out <strong>of</strong> the solar<br />

system by solar radiation pressure. This sweeping-out process would take an estimated 1000<br />

to 10,000 years (Brandt 1970). NASA is currently studying this process.

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