Lower thrust structure S/N 0000001 static structural test evaluation report Page: 25 of 53
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IV. EXPERIMENTAL RESULTS
The LTS was subjected to 12 static limit load combinations at room
temperature. Planned, and actual, test loads are shown in Figure 12. Generally,
Case 9 was the most critical load application. Loads for this Case consisted of
126 kips axial tension, .98 kip and .95 kip shear forces at the gimbal simulator,
and 28.22 kips and 28.49 kips compression forces at the pitch and yaw actuators,
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Lower thrust structure S/N 0000001 static structural test evaluation report, report, April 1, 1965; Sacramento, California. (https://digital.library.unt.edu/ark:/67531/metadc1024652/m1/25/: accessed March 20, 2019), University of North Texas Libraries, Digital Library, https://digital.library.unt.edu; crediting UNT Libraries Government Documents Department.