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Showing 1 to 1 of 1 for “"frequency response assurance criterion"”.

  1. Space Launch Environment and Vibration Testing

    … investigated through transient, random and shock response analysis to quantify the degree of over-testing and conclude that at least twice the base input was needed through sequential single-axis testing to envelop simultaneous tri-axis induced acceleration and stresses. This research further …

    auckland-ms Repository record for Space Launch Environment and Vibration Testing (opens in a new tab)