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🚧 This document is still being actively worked on and is subject to change. 🚧
| Authors |
|
| Responsible |
|
| Last Updated | 10/12/2025, 12:48:54 PM |
| Last Author | Kai Berszin |
<Insert the name of the Report>
| Subject | Description |
|---|---|
| Testing Model | Fully assembled EQM, Cable Setup, BioPayload (Todo: Check with PAY-Subteam) |
| Product Description | Random Vibration test with frequency range of 20-2000Hz |
| Test Reason | Test mechiancal integriy under cycling loads |
- Issue date: <Insert Date>
- Approved by: <Insert Name>
- Responsible Test Engineer: <Insert Name>
Random Vibration
Testing Equipment​
- Shakertable
- Structural Sensors (defined in Overview Strucutral Testing)
- EQM Adapter and EQM Model
- Locktie for the screws.
Test Method​
- The axial and lateral load factors should be taken from table 6-4 in the PUG and added with a margin of 6dB.
- The loads should be applied for 10 min.
- The Power Spectral Density should be according to the Table 4-10 and Figure 4.11 in the PUG from SpaceX.
- Duration: 1h
Check Condition and Requirements​
- We want to check the integrity with a low-level sine sweep performed before and after the test.
- Check the bolds after the test to verify, that they have not become lose. Todo: Insert table with the pre-tension on all bolds
Test Results​
<Describe the results of the test in a short fasion>
Test Judgement​
- Check for dynamic effects in the reaction and try to find out where they come from.
- We validate the integrity with a low-level Sine sweep afterwards.
- Check the tension on all bolds. They should not differ from the pre-tensioned value by more than 10%.
Appendix​
Photo of testing​
<Insert picture of the exact testing configuration>
Testing data​
<Insert a table or diagram of the exact output of the test (without intepretation)>