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NASA-LLIS-0669
Lessons Learned – Structural Laminate Composites for Space Applications
Year: 2000
Abstract: Practice:
The creation of reliable structural laminate composites for space applications requires precision design and manufacturing using an integrated, concurrent engineering approach. Since the final material characteristics are established at the same time the part or subassembly is fabricated, part design, fabrication development, and material characterization must proceed concurrently. Because composite materials are custom-tailored to meet structural requirements of the assembly, stringent inprocess controls are required to arrive at a configuration with optimum physical and material properties.
The creation of reliable structural laminate composites for space applications requires precision design and manufacturing using an integrated, concurrent engineering approach. Since the final material characteristics are established at the same time the part or subassembly is fabricated, part design, fabrication development, and material characterization must proceed concurrently. Because composite materials are custom-tailored to meet structural requirements of the assembly, stringent inprocess controls are required to arrive at a configuration with optimum physical and material properties.
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| contributor author | NASA - National Aeronautics and Space Administration (NASA) | |
| date accessioned | 2017-09-04T18:39:43Z | |
| date available | 2017-09-04T18:39:43Z | |
| date copyright | 03/07/2000 | |
| date issued | 2000 | |
| identifier other | ALCEQCAAAAAAAAAA.pdf | |
| identifier uri | http://yse.yabesh.ir/std;query=authoCA5893FD081D49A96159DD6EFDEC014A/handle/yse/221374 | |
| description abstract | Practice: The creation of reliable structural laminate composites for space applications requires precision design and manufacturing using an integrated, concurrent engineering approach. Since the final material characteristics are established at the same time the part or subassembly is fabricated, part design, fabrication development, and material characterization must proceed concurrently. Because composite materials are custom-tailored to meet structural requirements of the assembly, stringent inprocess controls are required to arrive at a configuration with optimum physical and material properties. | |
| language | English | |
| title | NASA-LLIS-0669 | num |
| title | Lessons Learned – Structural Laminate Composites for Space Applications | en |
| type | standard | |
| page | 8 | |
| status | Active | |
| tree | NASA - National Aeronautics and Space Administration (NASA):;2000 | |
| contenttype | fulltext |