NUCLEAR REACTOR FUEL ASSEMBLIES AND PROCESS FOR PRODUCTION
A nuclear fuel assembly for a nuclear reactor core, the fuel assembly having at least one fuel element including an elongated shell defining an interior volume, a lattice structure disposed within the interior volume, at least one flow channel extending through the lattice structure, at least one lattice site disposed in the lattice structure, and at least one fuel compact disposed within a corresponding one of the at least one lattice site, a first end cap including a boss having a first cross-sectional shape, the first end cap being affixed to a first end of the shell, and a second end cap including a first bore having a second cross-sectional shape, the second end cap being affixed to a second end of the shell, wherein the first cross-sectional shape of the boss is the same as the cross-sectional shape of the bore.
1 . A nuclear fuel assembly for a nuclear reactor core, comprising:
at least one fuel element comprising:
an elongated shell defining an interior volume and having a first end and a second end;
a lattice structure disposed within the interior volume;
at least one flow channel extending through the lattice structure;
at least one lattice site disposed in the lattice structure;
a first end cap including a boss having a first cross-sectional shape, the first end cap being affixed to the first end of the shell; and
a second end cap including a first bore having a second cross-sectional shape, the second end cap being affixed to the second end of the shell,
wherein the first cross-sectional shape of the boss is the same as the second cross-sectional shape of the bore.
2 . The fuel assembly of claim 1 , wherein the first and the second cross-sectional shapes are one of oval, triangular, rectangular, and polygonal.
3 . The fuel assembly of claim 1 , wherein the first and the second cross-sectional shapes are hexagonal.
4 . A nuclear thermal propulsion rocket engine comprising:
a nuclear reactor core, comprising:
a first fuel element and a second fuel element, each of the first fuel element and the second fuel element comprising:
an elongated shell defining an interior volume and having a first end and a second end;
a lattice structure disposed within the interior volume;
at least one flow channel extending through the lattice structure;
at least one lattice site disposed in the lattice structure;
a first end cap including a boss having a first cross-sectional shape, the first end cap being affixed to the first end of the shell, and
a second end cap including a first bore having a second cross-sectional shape, the second end cap being affixed to the second end of the shell,
wherein the first cross-sectional shape of the boss is the same as the second cross-sectional shape of the bore, and the boss of the first end cap of the first fuel element is disposed within the bore of the second end cap of the second fuel element.
5 . The rocket engine of claim 4 , wherein the first and the second cross-sectional shapes are one of oval, triangular, rectangular, and polygonal.
6 . The fuel assembly of claim 4 , wherein the first and the second cross-sectional shapes are hexagonal.