Patent Number: 047599111
Section: claims

1. A gas cooled nuclear fuel element, comprising a plurality of rigid porous cylinders suitably sized for coaxial positioning of each of the smaller of said cylinders within the next largest cylinder, wherein said cylinders are provided with varying quantities of fissionable nuclear fuel to maximize the total power production within the element. 2. The fuel element of claim 1, wherein said fuel element is designed for radial gas flowthrough and axial gas outflow. 3. The fuel element of claim 1, wherein said fuel element is provided with the nuclear fuel uranium carbide. 4. The fuel element of claim 1, wherein said fuel element is provided with the nuclear fuel plutonium carbide. 5. The fuel element of claim 1, wherein said fuel element is provided with the nuclear fuel americium carbide. 6. The fuel element of claim 1, wherein said fuel element is provided with the nuclear fuel uranium dicarbide. 7. The fuel element of claim 1, wherein said porous cylinders have pores in the range of 0.5 to 5.0 millimeters. 8. The fuel element of claim 1, wherein said porous cylinders are formed from reticulated vitreous carbon. 9. The fuel element of claim 1, further comprising a protective layer of carbon on said cylinders. 10. The fuel element of claim 1, further comprising a protective layer of zirconium carbide on said cylinders. 11. A process for preparing a gas cooled nuclear fuel element, comprising: a. selecting a retriculated vitreous carbon skeleton of appropriate pore and ligament size;  b. depositing a fissile material on said skeleton; and  c. subjecting said coated skeleton to high temperature whereby said fissile material is changed to its carbide form. 12. The process of claim 11, further comprising depositing a protective layer of carbon on said coated skeleton. 13. The process of claim 12, further comprising depositing a protective layer of zirconium carbide over said carbon layer. 14. The process of claim 11, wherein said depositing of fissile material is accomplished by vapor deposition coating. 15. The process of claim 11, wherein the pore size of said skeleton ranges from 0.5 to 5.0 millimeters.