CUBICS

Responsible: @Abegail Gagelonia
Accountable: @Abegail Gagelonia
Consulted: @Alice Nguyen , @Saksham Verma , @Ben Harbarenko
Informed: Mechanical Team

What: Please select three feasible release mechanism candidates and create a detailed documentation for all them in the file created by @Abegail Gagelonia: https://docs.google.com/document/d/1KQu0ZAUYY7AGOVG6KH6xUe7zpoQm9z7J1GobwZrREGQ/edit.
Keep in mind the requirements of the satellite which directly affect the release mechanisms and account for factors such as reliability, power usage, thermal susceptibility and more. Feel free to use the decision matrix to understand what you have to account for: https://docs.google.com/spreadsheets/d/134AGhXuuVQ-dcDMZIZ2bac72vwPK9nmd1KrHs49GeqI/edit#gid=0

Slides 39-41 of the attached PDF / https://drive.google.com/drive/search?q=release%20mechanism (07 CCP-CSA-00017-WEB-PPT-Rev- Mechanical and Material), also provides some off-the-shelf solutions mentioned by the CSA.

Lastly, after you are done, please inform @Jack Fraser so that he can populate the decision matrix.

Why: We need to come up with a better and more reliable release mechanism solution than EX2