Orbit debris removal and asset protection assembly
View Patent ↗An orbital debris removal assembly is provided. The orbital debris removal and asset protection assembly includes a plurality of spaced layers of netting. Each netting layer includes a plurality of sub-layers of meshed composite fibers that are configured and arranged to break up debris that comes in contact with the assembly.
1. An orbital debris removal and asset protection assembly comprising:
a plurality of spaced layers of netting, each netting layer including sub-layers of meshed composite fibers configured and arranged to break up debris that comes in contact with the assembly;
a spacecraft coupled to the plurality of spaced layers of netting;
at least one deployable boom coupled to the spacecraft; and
at least one thruster coupled to the rotational boom to selectively position the spacecraft.
2. The orbital debris removal and asset protection assembly of claim 1 , further comprising:
each spaced layer having a fiber mesh density, the fiber mesh density of one layer of the plurality of spaced layers having a different fiber mesh density of at least one other layer of the plurality of spaced layers.
3. The orbital debris removal and asset protection assembly of claim 1 , further comprising:
the composite fibers that make up the meshed fibers have a select thickness, the thickness of the composited fibers of one layer of the plurality of spaced layers being different than the thickness of the fibers in at least one other layer of the plurality of spaced layers.
4. The orbital debris removal and asset protection assembly of claim 1 , further comprising;
the plurality of spaced layers of netting at least partially being in a sphere shape.
5. The orbital debris removal and asset protection assembly of claim 1 , further comprising:
frame members configured and arranged to hold to the plurality of spaced layers of netting.
6. The orbital debris removal and asset protection assembly of claim 5 , wherein the frame members are configured and arranged to be folded up to put the orbital debris removal assembly in a stowed position.
7. The orbital debris removal and asset protection assembly of claim 1 , wherein the composite fibers are at least one of para-aramid, polyolefin, ceramic and Dyneema fiber bundles.
8. The orbital debris removal and asset protection assembly of claim 1 , further comprising:
the spacecraft further configured to selectively deploy the plurality of spaced layers of netting and store the plurality of spaced layers of netting.
9. An orbital debris removal and asset protection assembly comprising:
a spacecraft configured to navigate in space;
a plurality of spaced netting layers coupled to the spacecraft, each netting layer including meshed fibers;
at least one deployable boom coupled to the spacecraft; and
at least one thruster coupled to the rotational boom to selectively position the spacecraft.
10. The orbital debris removal and asset protection assembly of claim 9 , wherein the meshed fibers are composite fibers.
11. The orbital debris removal and asset protection assembly of claim 9 , further comprising:
frame members coupled to the spacecraft, the frame member further configured and arranged to form the plurality of the spaced netting layers.
12. The orbital debris removal and asset protection assembly of claim 11 , wherein the frame members from the spaced netting layers in at least a partial sphere shape.
13. The orbital debris removal and asset protection assembly of claim 9 , further comprising:
the plurality of spaced netting layers having an outer layer, an inner layer and at least one mid layer between the outer layer and the inner layer,
each layer having a select fiber mesh density, the fiber density of the meshed fibers in each spaced layer increasing from the outer layer to the inner layer.
14. The orbital debris removal and asset protection assembly of claim 9 , further comprising:
the plurality of spaced netting layers having an outer layer, an inner layer and at least one mid layer between the outer layer and the inner layer; and
the meshed fibers in each layer having a select thickness, the thickness of the meshed fibers in each spaced layer decreasing from the outer layer to the inner layer.
15. The orbital debris removal and asset protection assembly of claim 9 , wherein each netting layer, includes a plurality of sub-layers of meshed fibers.
16. The orbital debris removal and asset protection assembly of claim 15 , further comprising:
a plurality of connecting fibers configured and arranged to couple the sub-layers together.
17. The orbital debris removal assembly and asset protection assembly of claim 15 , wherein at least one sub-layer of the plurality of sub-layers has a different fiber spacing than at least one other sub-layer.
18. The orbital debris removal assembly and asset protection assembly of claim 15 , wherein at least one sub-layer of the plurality of sub-layers has a different fiber thickness than at least one other sub-layer.
19. An orbital debris removal and asset protection assembly comprising:
a plurality of spaced layers of netting formed in at least a partial sphere shape, each netting layer including meshed composite fibers, the plurality of spaced layers of netting having an outer layer, an inner layer and at least one mid layer between the outer layer and the inner layer, each layer having a select fiber density, the fiber density of the meshed composite fibers in each spaced layer varying from the outer layer to the inner layer;
a spacecraft coupled to the plurality of spaced layers;
at least one deployable boom coupled to the spacecraft; and
at least one thruster coupled to the rotational boom to selectively position the spacecraft at a desired location in space.
20. The orbital debris removal and asset protection assembly of claim 19 , the plurality of spaced layers of netting having a first section and a second section, the first and section conformed and arranged to form a complete sphere when deployed.
21. The orbital debris removal and asset protection assembly of claim 19 , wherein the meshed composite fibers in each layer have a select thickness, the thickness of the meshed fibers in each spaced layer decreasing from the outer layer to the inner layer.
22. The orbital debris removal and asset protection assembly of claim 19 , further comprising:
a plurality of frame members configured and arranged to selectively space the plurality spaced layers of netting.
23. The orbital debris removal and asset protection assembly of claim 22 , wherein the frame members are further configured to place the plurality of spaced layers of netting in a deployed position and a storage position.
24. The orbital debris removal and asset protection assembly of claim 22 , further comprising:
at least one deployable member configured to selectively deploy the plurality of spaced layers of netting.
25. The orbital debris removal and asset protection assembly of claim 19 , further comprising:
a controller configured to control the thrusters of the spacecraft;
a transceiver in communication with the controller to provided communications to the controller; and
at least one sensor in communication with the controller.
26. The orbital debris removal and asset protection assembly of claim 25 , wherein the at least one sensor is at least one of an impact sensor and a velocity sensor.
27. The orbital debris removal and asset protection assembly of claim 19 , wherein at least one of the plurality of spaced layers is made of a plurality of meshed composite fiber sub -layers.