Hybrid Rocket Engine Fuel Grains with Radial Energy Compositional Variations
A method of making a fuel grain for a hybrid rocket engine includes deposing beads of fuel grain material onto mandrel using additive manufacturing to form a cylindrical fuel grain, each bead including a polymer based rocket fuel material and a nanoscale metallic material. The deposing includes deposing multiple, adjacent beads to form concentric layers of beads, wherein a composition of the beads of the fuel grain material differs between the beads of a first layer and the beads of a second layer of the fuel grain.
1 . (canceled)
2 . A method of making a propellant for a rocket engine, the method comprising:
deposing beads of an energetic material adjacent to one another using additive manufacturing to form a cylindrical propellant defining a combustion port extending axially therethrough, the deposing comprising:
deposing multiple, adjacent beads of different composition to form concentric layers of beads, wherein a composition of the beads of the energetic material differs between the beads of a first layer and the beads of a second layer of the cylindrical propellant.
3 . The method of claim 2 , wherein the energetic material comprises a polymer.
4 . The method of claim 3 , wherein the polymer comprises a thermoplastic polymer.
5 . The method of claim 3 , wherein the energetic material further comprises metallic particles.
6 . The method of claim 5 , in which deposing multiple beads comprises deposing beads comprising between 75% and 95% by weight of the polymer and between 5% and 25% by weight of the metallic particles.
7 . The method of claim 5 , wherein a weight percentage of the metallic particles or a size of the metallic particles in the beads of the energetic material differs between the beads of the first layer and the beads of the second layer of the cylindrical propellant.
8 . The method of claim 5 , wherein the beads of an innermost one of the concentric layers have a greater weight percentage of the metallic particles as compared to the beads of an outermost one of the concentric layers.
9 . The method of claim 5 , wherein the beads of an innermost one of the concentric layers have smaller metallic particles as compared to the beads of an outermost one of the concentric layers.
10 . The method of claim 5 , wherein the metallic particles are passivated metallic particles.
11 . The method of claim 2 , comprising deposing the beads using a single deposition head.
12 . The method of claim 11 , in which deposing each layer of beads comprises changing an amount of the metallic particles provided to the single deposition head between deposition of the beads of the first layer and deposition of the beads of the second layer.
13 . The method of claim 12 , in which changing the amount of the metallic particles comprises varying a rate at which the metallic particles is provided to the single deposition head.
14 . The method of claim 2 , comprising deposing the beads of the first layer using a first deposition head and deposing the beads of the second layer using a second deposition head, comprising supplying a first composition of energetic material to the first deposition head and a second composition of energetic material to the second deposition head.
15 . The method of claim 2 , comprising encasing the cylindrical propellant in a cover.
16 . The method of claim 2 , wherein an innermost one of the concentric layers has a ribbed texture.
17 . The method of claim 2 , comprising adjusting a dimension of the beads between deposing a first bead and an adjacent second bead.
18 . The method of claim 2 , wherein the composition of the beads of the energetic material differs between adjacent beads in a single one of the concentric layers.