MOLA Feet/Support Panel Interface Random Vibration Analysis Results

This area presents the analysis results of the Feet/Support Panel Interface (see the exploded view for details).

Random analytical response due to the MOLA random vibration input

The responses of this interface are presented here. These responses are due to the random vibration of the entire MOLA instrument FEM. (The MOLA input spec is also available.)

Because the feet/support panel interface will not be random tested, no test specification was derived from the anlaytical responses.

Back to the Random Response Page.
Back to the MOLA Random Vibration Page.
Back to the MOLA Mechanical Analysis Page.

This page is maintained by Ryan Simmons, at Ryan.Simmons@nasa.gov.
This page was last updated on September 8, 1995.