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Fabrication of very-low-density, high-stiffness carbon fiber/aluminum hybridized composite with ultra-low density and high stiffness (m-11)
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Suzuki, Tomoo |
| Copyright Year | 1993 |
| Description | Fabrication of a composite material with ultra-low density and high stiffness in microgravity is the objective of the investigation. The composite structure to be obtained is a random three-dimensional array of high modulus, short carbon fibers bonded at contact points by an aluminum alloy coated on the fibers. The material is highly porous and thus has a very low density. The motivation toward the investigation, simulation experiments, choice of the component materials, and on-flight experiment during ballistic trajectory of a NASDA rocket, are described. |
| File Size | 291610 |
| Page Count | 8 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19940009270 |
| Archival Resource Key | ark:/13960/t7fr4sv8f |
| Language | English |
| Publisher Date | 1993-08-01 |
| Access Restriction | Open |
| Subject Keyword | Materials Processing Fabrication Carbon Fibers Cermets Spaceborne Experiments Fiber Composites Low Density Materials Aluminum Alloys Metal Matrix Composites Stiffness Porosity Composite Structures Microgravity Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Technical Report |
