Marshall Technical Reports Server

Subject: Stresses and Loads


Number of records: 14.

NASA/SP-8072, Acoustic loads generated by the propulsion system, NASA SPACE VEHICLE DESIGN CRITERIA (Structures), NASA (Washington, DC, United States), June,1971, pp. 54, Format(s): PDF 2629k

NASA/SP-8099, Houbolt, J. C., Combining ascent loads, NASA SPACE VEHICLE DESIGN CRITERIA (Structures), NASA (Washington, DC, United States), June,1972, pp. 36, Format(s): PDF 1597k

NASA/TM-208594, Brown, A.M., Comprehensive Structural Dynamic Analysis of the SSME/AT Fuel Pump First-Stage Turbine Blade, Structures and Dynamics Laboratory, Science and Engineering Directorate, NASA Marshall Space Flight Center, AL 35812, August 1998, pp. 20, Format(s): PDF 1039k

NASA/TP-3589, Herda, D.A. and Gross*, R.S., High Pressure Oxidizer Turbopump (HPOTP) Inducer Dynamic Design Environment, Structures and Dynamics Laboratory, Science and Engineering Directorate. NASA Marshall Space Flight Center, AL 35812 and *Auburn University, November 1995, pp. 27, Format(s): PDF 351k

NASA/SP-8046, Jones*, R. H., Landing Impact Attenuation For Non-Surface-Planing Landers, NASA SPACE VEHICLE DESIGN CRITERIA (Structures), NASA (Washington, DC, United States), *Hughes Aircraft Co. (Culver City, CA, United States), April,1970, pp. 47, Format(s): PDF 2502k

NASA/SP-8009, Propellant slosh loads, NASA SPACE VEHICLE DESIGN CRITERIA (Structures), NASA (Washington, DC, United States), August,1968, pp. 30, Format(s): PDF 2591k

NASA/SP-8022, Goldman*, R.L., Staging loads - Space vehicle design criteria, NASA SPACE VEHICLE DESIGN CRITERIA (Structures), NASA (Washington, DC, United States), NASA Langley Research Center and *Research Institute for Advanced Studies, February,1969, pp. 30, Format(s): PDF 1493k

NASA/TP-2003-212257, Brown, A.M. and McGhee, D.S., Statistical Evaluation and Improvement of Methods for Combining Random and Harmonic Loads, George C. Marshall Space Flight Center , Marshall Space Flight Center, AL 35812, National Aeronautics and Space Administration, Washington, DC 20546-0001, February 2003, pp. 32, Format(s): PDF 288k

NASA/SP-8082, Stress-corrosion cracking in metals, NASA SPACE VEHICLE DESIGN CRITERIA (Structures), NASA Langley Research Center (Hampton, VA, United States), August,1971, pp. 42, Format(s): PDF 4970k

NASA/SP-8050, Archer*, J. S., Structural Vibration Prediction, NASA SPACE VEHICLE DESIGN CRITERIA (Structures), NASA (Washington, DC, United States), *TRW Systems Group/TRW Inc., June,1970, pp. 41, Format(s): PDF 2473k

NASA/TM-108542, Lee, H.M., Testing for Random Limit Load Versus Static Limit Load, Structures and Dynamics Laboratory, Science and Engineering Directorate. NASA Marshall Space Flight Center, AL 35812, September 1997, pp. 36, Format(s): PDF 319k

NASA/SP-8030, Transient Loads From Thrust Excitation, NASA SPACE VEHICLE DESIGN CRITERIA (Structures), NASA (Washington, DC, United States), NASA Langley Research Center (Hampton, VA, United States), February,1969, pp. 28, Format(s): PDF 1320k

NASA/SP-8077, Ostrem, F.E., Transportation and handling loads, NASA SPACE VEHICLE DESIGN CRITERIA (Structures), NASA Langley Research Center (Hampton, VA, United States), September,1971, pp. 48, Format(s): PDF 3035k

NASA/SP-8035, Wind Loads During Ascent, NASA SPACE VEHICLE DESIGN CRITERIA (Structures), NASA (Washington, DC, United States), June,1970, pp. 36, Format(s): PDF 2122k

This list was generated on Thu Jan 17 00:10:02 CST 2008.