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  • 1
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    Random Data; Analysis and Measurement Procedures (1986)
    John Wiley & Sons, 608 pp.
    In:  Basel, 375 pp., John Wiley & Sons, 608 pp., vol. 96, pp. 225, (ISBN 3-7643-7011-4)
    Details
    Publication Date: 1986
    Keywords: Textbook of engineering ; Data analysis / ~ processing ; Textbook of geophysics ; Correlation ; Spectrum ; Non-linear effects ; Time series analysis ; random
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    BIBLIOGRAPHY SEISMOLOGY
  • 2
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    Random Data; Analysis and Measurement Procedures (1971)
    John Wiley & Sons, 407 pp.
    In:  Basel, 375 pp., John Wiley & Sons, 407 pp., vol. 96, pp. 225, (ISBN 3-7643-7011-4)
    Details
    Publication Date: 1971
    Keywords: Textbook of engineering ; Data analysis / ~ processing ; Textbook of geophysics ; Correlation ; Spectrum ; Non-linear effects ; Time series analysis ; random
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    BIBLIOGRAPHY SEISMOLOGY
  • 3
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    Acoustic Load Considerations for Spacecraft Structures (1986)
    In:  CASI
    Details
    Publication Date: 2012-08-15
    Description: An analytical model to predict the space averaged sound pressure levels in the payload bay of the Space Shuttle orbiter vehicle at lift-off was developed. A modified form of the model can also be used to predict vibration levels of the orbiter mid fuselage and to evaluate noise control concepts for the interior of the proposed Aft Cargo Carrier (ACC). The analytical model is presented and predicted payload bay sound pressure levels are compared with launch data for an empty bay. Estimated and measured sound pressure levels for regions above large diameter payloads are found to be significantly higher than those for the empty bay. The use of helium as a purge gas to reduce sound pressure levels in the ACC is proposed.
    Keywords: SPACE TRANSPORTATION
    Type: ESA Proceedings of an International Conference on Spacecraft Structures; p 133-143
    Format: text
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    NASA TECHNICAL REPORTS
  • 4
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    Analytical and experimental evaluations of Space Shuttle TPS tile vibration response (1982)
    In:  Other Sources
    Details
    Publication Date: 2011-08-18
    Description: Analytical studies and laboratory experiments have been performed to evaluate the vibration response of the Space Shuttle Thermal Protection System (TPS) tiles due to the intense rocket generated acoustic noise during lift-off. The TPS tiles are mounted over the exterior of the Space Shuttle Orbiter structure through Strain Isolation Pads (SIP) which protect the tiles from thermal induced shear loads at their interface. The analytical predictions indicate that the response of a typical tile is governed by the structural vibration inputs through the SIP under the tile at frequencies below 250 Hz, and by the direct acoustic excitation over the exterior surface of the tile at frequencies above 250 Hz. An evaluation of the laboratory test data for this same tile, in which conditioned (partial) coherent output spectral analysis procedures were used, leads to exactly the same conclusion. The results demonstrate the power of conditioned spectral analysis procedures in identifying vibration response mechanisms when two or more of the inputs are highly correlated.
    Keywords: SPACECRAFT DESIGN, TESTING AND PERFORMANCE
    Type: Journal of Sound and Vibration; 83; July 8
    Format: text
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    NASA TECHNICAL REPORTS
  • 5
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    Handbook for Dynamic Data Acquisition and Analysis - IES Recommended Practices 012.1 (1994)
    In:  Other Sources
    Details
    Publication Date: 2018-06-08
    Description: The original motivation for this Handbook came from personnel of The Aerospace Corporation (TAC), who are technical advisors to the Air Force Space and Missile Systems Center. Over the preceding two decades, TAC has observed a seemingly endless series of errors and anomalies in the acquisition and analysis of structural dynamic and aeroacoustic data.
    Format: text
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    NASA TECHNICAL REPORTS
  • 6
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    Guidelines for Dynamic Environmental Criteria: An Invitatin to Participate in Their Development (1994)
    In:  Other Sources
    Details
    Publication Date: 2018-06-08
    Description: The development of guidelines for dynamic design and test criteria has recently been ititiated under the sponsorship of the Office of Safety and Mission Quality, NASA Headquarters.
    Format: text
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    NASA TECHNICAL REPORTS
  • 7
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    Guidelines for Dynamic Environmental Criteria: An Invitation to Participate in Their Development (1993)
    In:  Other Sources
    Details
    Publication Date: 2018-06-08
    Description: The development of guidelines for dynamic design and test criteria has recently been initiatedunder the sponsorship of the Office of Safety and Mission Quality, NASA Headquarters. To ensurethat all current methods of criteria derivation are included, an invitation is being extended to allpractitioners to participate in the preparation of these guidelines.
    Type: 64th Shock and Vibration Symposium; Ft. Walton Beach, FL; United States|Proc., 64th Shock and Vibration Symposium
    Format: text
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    NASA TECHNICAL REPORTS
  • 8
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    The Proposed NASA Pyroshock Test Criteria Standard - Part I (1996)
    In:  Other Sources
    Details
    Publication Date: 2018-06-08
    Description: The National Aeronautics and Space Administration has traditionally left the task of specifying design and test criteria to each of the several NASA Centers. Faced with the wide variety fo resulting criteria used for resolving similar or identical problems, the NASA Office of Chief Engineer initiated a program to develop consistent NASA-wide standards if the various NASA Centers could agree to a set of common requirements.
    Format: text
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    NASA TECHNICAL REPORTS
  • 9
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    Spectral analysis of nonstationary spacecraft vibration data (1965)
    In:  CASI
    Details
    Publication Date: 2019-05-29
    Description: Procedures for describing and analyzing frequency composition of spacecraft launch vibration data
    Keywords: STRUCTURAL MECHANICS
    Type: NASA-CR-341
    Format: application/pdf
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    NASA TECHNICAL REPORTS
  • 10
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    The development of vibration test specifications for flight vehicle components. (1966)
    In:  Other Sources
    Details
    Publication Date: 2019-05-30
    Description: Vibration test specifications for flight vehicle components developed from broad engineering viewpoint
    Keywords: SPACE VEHICLES
    Type: JOURNAL OF SOUND AND VIBRATION
    Format: text
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    NASA TECHNICAL REPORTS
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