AAWSAP DIRD, Materials for Advanced Aerospace Platforms, January 2010
DOW-UAP-D120 · page 3 of 27
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UNCLASSIFIED//FOR OFFI@IAl W&lii 9PU.Y Contents Introduction ...........................................................................................................iv Launch Vehicles ................................................................................................. 1 Reusable Crew Modules...................................................................................... 9 Reusable Single-Stage-to-Orbit Vehicles ...................................................... 10 Advanced Al Alloys ....................................................................................... 11 Polymer Matrix Composites.......................................................................... 11 Al Matrix Composites.................................................................................... 12 Ti Alloys ....................................................................................................... 12 Ti Matrix Composites.................................................................................... 14 Ni-base Alloys .............................................................................................. 16 Refractory Metal Alloys ................................................................................ 18 Ceramic Matrix Composites .......................................................................... 18 Carbon-Carbon Composites .......................................................................... 19 Titanium Aluminides .................................................................................... 20 Propulsion Systems.......................................................................................... 21 Summary and Recommendations ..................................................................... 22 Figures 1. Schematic Diagram of Friction Stir Welding ....................................................... 2 2. Specially Modified 747 Transporter Unloading a Boeing 787 Composite Fuselage Barrel Section ..................................................................................... 4 3. Micrograph Showing Phase Formation at the Surface of a Ti Alloy That has Been Exposed to Air at Elevated Temperature ................................................. 13 4. Cross-Section Micrograph of a Ti Matrix Composite.......................................... 15 Tables 1. Potential Materials by Use Temperature Regime and Property ......................... 10 2. Example of Properties of Ti Matrix Composites ................................................ 14 iii UNCLASSIFIED//FOR 0FFI€1Ak Uili ,u1k¥