The application is the floor of an aircraft. The floor is a sandwich construction, laminiates above/below a core. I have two property reports on the tape, but my NASTRAN run indicates compressive stress in interior plys in the 90 degree (matrix) direction near holes. So I am concerned about failure in matrix direction in compression. But I can't find any test data for that strength value. But the tape is a category 5 material and (I believe) that means the material is in general use and the properties are well established. I have modulus and strength in 0 deg (compression and tension) and in 90 deg (only tension), and am missing strength in 90 degree compression.
Currently, my margin of safety for compression 90 degree failure mode is based on scaling the compression strength of a S-2 bidirectional fabric. But I recognize that the 90 degree compression strength of a uni-directional tape is not similar to a bi-direction weave. But I don't have another number to use.
I'm not very familiar with composite materials, but since it is a cat V material I'm supprised that I can't find the properties somewhere.