Number of records: 6.
NASA/TM-2008-215253, Ferebee, R.C. and Clayton, J. and Alldredge, D. and Irvine, T., An Alternative Method of Specifying Shock Test Criteria, George C. Marshall Space Flight Center, Marshall Space Flight Center, AL 35812, National Aeronautics and Space Administration, Washington, DC 20546–0001 , April 2008, pp. 44, Format(s): PDF 1552k
NASA/TM-2004-213170, Steeve, B.E. and Kapernick, R.J., Design Development Analyses in Support of a Heat Pipe-Brayton Cycle Heat Exchanger, George C. Marshall Space Flight Center , Marshall Space Flight Center, AL 35812, National Aeronautics and Space Administration, Washington, DC 20546-0001, May 2004, pp. 32, Format(s): PDF 4501k
NASA/TP—2007–214960, Hull, P.V. and Tinker, M.L. and Dozier, G.V., Evolutionary Optimization of a Geometrically Refined Truss, George C. Marshall Space Flight Center, Marshall Space Flight Center, AL 35812, National Aeronautics and Space Administration, Washington, DC 20546–0001, June 2007, pp. 32, Format(s): PDF 11129k
NASA/TM-2005-213609, Steeve, B.E., Safe Affordable Fission Engine- (SAFE-) 100a Heat Exchanger
Thermal and Structural Analysis, George C. Marshall Space Flight Center , Marshall Space Flight Center, AL 35812, National Aeronautics and Space Administration, Washington, DC 20546-0001, March 2005, pp. 48, Format(s): PDF 7525k
NASA/CR-2005-214006, Wawrzynek, P.A. and Carter, B.J. and Banks-Sills, L., The M-Integral for Computing Stress in Generally Anisotropic Materials, George C. Marshall Space Flight Center, Marshall Space Flight Center, AL 35812, July, 2005, pp. 88, Format(s): PDF 2422k
NASA/TP—2007–214962, Hull, P.V. and Tinker, M.L., Topology Synthesis of Structures Using Parameter Relaxation
and Geometric Refinement, George C. Marshall Space Flight Center, Marshall Space Flight Center, AL 35812, National Aeronautics and Space Administration, Washington, DC 20546–0001, June 2007, pp. 28, Format(s): PDF 7554k
This list was generated on Thu May 28 09:05:30 CDT 2009.