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🚧 This document is still being actively worked on and is subject to change. 🚧
| Responsible |
|
| Last Updated | 10/12/2025, 12:48:54 PM |
| Last Author | Kai Berszin |
Dimensional Verification
| Subject | Description |
|---|---|
| Testing Model | Flight Model |
| Product Description | Dimensional Verification of the Satellie |
| Test Reason | Verification of the Assembly plan and test if all parts have the right dimensions |
- Issue date: <Insert Date>
- Approved by: <Insert Name>
- Responsible Test Engineer: <Insert Name>
Dimensional Verification Test
Testing Equipment​
- None -> except all original parts of the satellite and the tools described in the Assembly plan
Test Method​
- The test is conducted in a clean-room according to the Assembly plan.
- Every action on the satellite should be done with two people. One person is performing the task and the other one is checking it. If we have paper that should be filled in during the assembly to document it, they should also be filled out.
- Duration: 4h with the subcomponent assembled
Check Condition and Requirements​
- Parts that should not touch should have at least 3mm of clearance
- No part that shouldn't be under tension should need force to place it.
- The scews should also be tested if mentioned in the assembly manual.
Test Results​
<Describe the results of the test in a short fasion>
Test Judgement​
The criterias apply to all components
- Parts that should not touch should have at least 3mm of clearance
- No part that shouldn't be under tension should need force to place it. (This applies to nothing except the screws and the connection between the antenna release mechanism and the antenna themself.)
Appendix​
Photo of testing​
<Insert picture of the exact testing configuration>