Evolution of technologies applied to space and aeronautic structures
Abstract
Advanced materials in aerospace structures and their use in reusable launch vehicles are discussed. It is found that composite materials can be used for structures with temperatures up to 400 C, and for most structures with heat shielding. For structures with temperatures up to 1000 C, metals such as Norsial, based on rene alloys could be used. It is concluded that a combination of silicon and carbon composites with Aerocoat/TH hydrotranspiration heat shielding give a heat flux resistant structure with no thermal dilation problems.
- Publication:
-
In CNES The Future of Launchers in Europe
- Pub Date:
- 1982
- Bibcode:
- 1982cnes.rept..409A
- Keywords:
-
- Aerospace Engineering;
- Composite Materials;
- Heat Resistant Alloys;
- Technology Assessment;
- Technology Utilization;
- Cost Reduction;
- Heat Flux;
- Reentry Shielding;
- Reentry Vehicles;
- Refractory Metal Alloys;
- Rene 41;
- Reusable Launch Vehicles;
- Launch Vehicles and Space Vehicles