CNT-based signature control material
A radar absorbing composite includes a (CNT)-infused fiber material disposed in at least a portion of a matrix material. The composite absorbs radar in a frequency range from about 0.10 Megahertz to about 60 Gigahertz. The CNT-infused fiber material forms a first layer that reduces radar reflectance and a second layer that dissipates the energy of the radar. A method of manufacturing this composite includes disposing a CNT-infused fiber material in a portion of a matrix material with a controlled orientation of the CNT-infused fiber material within the matrix material, and curing the matrix material. The composite can be formed into a panel which is adaptable as a structural component of a transport vessel or missile for use in stealth applications.
1. A radar absorbing composite comprising a carbon nanotube-infused fiber material disposed in at least a portion of a matrix material, the composite being capable of absorbing radar in a frequency range from between about 0.10 Megahertz to about 60 Gigahertz, the carbon nanotube-infused fiber material forming a first layer that reduces radar reflectance and a second layer that dissipates the energy of the absorbed radar.
2. The composite of claim 1 further comprising a plurality of transition metal nanoparticles.
3. The composite of claim 2 , wherein the nanoparticles comprise iron.
4. The composite of claim 1 , further comprising a plurality of additional layers between the first layer and the second layer.
5. The composite of claim 4 , wherein the plurality of additional layers comprises a stepped gradient of increasing carbon nanotube density on the carbon nanotube-infused fiber material from the first layer down to the second layer.
6. The composite of claim 4 , wherein the plurality of additional layers comprises a continuous gradient of increasing carbon nanotube density on the carbon nanotube-infused fiber material from the first layer down to the second layer.
7. The composite of claim 1 , wherein the first layer and the second layer comprise separate carbon nanotube-infused fiber materials.
8. The composite of claims 7 , wherein the first layer comprises a carbon nanotube-infused glass fiber material.
9. The composite of claim 7 , wherein the second layer comprises a carbon nanotube-infused carbon fiber material.
10. The composite of claim 1 , wherein the carbon nanotubes are present in a range between about 0.001% by weight to about 20% by weight of the composite.
11. The composite material of claim 1 , wherein the carbon nanotube-infused fiber material comprises a fiber material selected from glass, carbon, and ceramic.
12. The composite material of claim 1 , wherein the carbon nanotubes infused on the fiber material have a controlled orientation within the composite.
13. A method of manufacturing a radar absorbing composite, the composite comprising a carbon nanotube-infused fiber material disposed in at least a portion of a matrix material, the composite being capable of absorbing radar in a frequency range from between about 0.10 Megahertz to about 60 Gigahertz, the carbon nanotube-infused fiber material forming a first layer that reduces radar reflectance and a second layer that dissipates the energy of the absorbed radar, the method comprising disposing a carbon nanotube-infused fiber material in a portion of a matrix material with a controlled orientation of the carbon nanotube-infused fiber material within the matrix material, and curing the matrix material, wherein the controlled orientation of the carbon nanotube-infused fiber material controls the relative orientation of carbon nanotubes-infused thereon.
14. A panel comprising a composite, the composite comprising a carbon nanotube-infused fiber material disposed in at least a portion of a matrix material, the composite being capable of absorbing radar in a frequency range from between about 0.10 Megahertz to about 60 Gigahertz, the carbon nanotube-infused fiber material forming a first layer that reduces radar reflectance and a second layer that dissipates the energy of the absorbed radar, the panel being adaptable as a structural component of a transport vessel or missile for use in stealth applications.
15. A transport vessel comprising the panel of claim 14 , wherein the carbon nanotubes infused on the fiber material have a controlled orientation within the composite material.
16. The transport vessel of claim 15 , wherein the transport vessel is selected from a boat, a plane, and a ground vehicle.
17. A projectile comprising the panel of claim 14 , wherein the carbon nanotubes infused on the fiber material have a controlled orientation within the composite material.