Next: 2.2.3 Thermal
Up: 2.2.2 Mechanical
Previous: 2.2.2.1 ACIS Structural Design
ACIS has undergone extensive preflight structural and dynamic testing. The ACIS team has prepared models of the mechanical and dynamic behavior of the instrument and detailed analyses of these models have been carried out to verify the models against the test data. As a full description of this testing is out of the scope of this Operations manual we refer the reader to the extensive list of ACIS provided technical documents listed in Table 2.1.
MIT Doc. # | Rev. | Name |
36-01303 | B | DEA, DPA & Support Structure Test Procedure |
36-01501 | 01 | Verification Test & Assessment Reports |
36-01504 | A | SS Stress & Vibration Analysis |
36-01505 | B | MIT Fracture & Fatigue Analysis |
36-01510.0094 | CEI Verification Report Summary - Random Vibration | |
36-01510.0095 | " " - Design Loads | |
36-01510.0096 | " " - Component Loads | |
36-01510.0097 | " " - System Load Factors | |
36-01520.0010 | ICD Verification Report Summary -Mass Properties | |
36-01520.0038 | " " - Natural Frequency | |
36-01520.0039 | " " - Random Vibration | |
36-01502 | 01 | Technical Analysis & Models |
36-01502.01 | A | LMA Dynamic Analyses & Tests |
36-01502.02 | A | LMA Stress Analysis |
John Nousek