Number of records: 4.
NASA/CP-3287, Aluminum-Lithium Alloys for Aerospace Applications Workshop, Bhat, B.N. and Bales, T.T. and Vesely Jr., E.J., In proceedings of Aluminum-Lithium Alloys for Aerospace Applications Workshop, pp. 363, Marshall Space Flight Center, December, 1994 Format(s): PDF 17864k>
NASA/TM-211546, Chen*, P.S. and Stanton, W.P., Artificial Aging Effects on Cryogenic Fracture Toughness of the Main Structural Alloy for the Super Lightweight Tank, George C. Marshall Space Flight Center Marshall Space Flight Center, AL 35812, National Aeronautics and Space Administration Washington, DC 20546-0001, Prepared for Engineering Directorate, Materials, Processes, and Manufacturing Department *IIT Researc, February 2002, pp. 28, Format(s): PDF 13684k
NASA/TM-211547, Chen*, P.S. and Stanton, W.P., Cryogenic Fracture Toughness Improvement for the Super Lightweight Tank's Main Structural Alloy, George C. Marshall Space Flight Center Marshall Space Flight Center, AL 35812, National Aeronautics and Space Administration Washington, DC 20546-0001, Prepared for the Engineering Directorate, Materials, Processes, and Manufacturing Department * IIT Res, February 2002, pp. 20, Format(s): PDF 4650k
NASA/SP-8040, Tiffany*, C.F., Fracture Control of Metallic Pressure Vessels, NASA SPACE VEHICLE DESIGN CRITERIA (Structures), NASA (Washington, DC, United States), *Boeing Co. (Seattle, WA, United States), May,1970, pp. 65, Format(s): PDF 4610k
This list was generated on Thu Jan 17 00:07:03 CST 2008.