Space Mission Louver System

This project involved a louver-style thermal and mechanical system concept for a space mission context.

The page uses selected mechanism visuals, report figures, and PDFs to explain the design without publishing raw working files.

Thermal louver systems need controlled opening and closing behaviour while satisfying mechanical and thermal constraints.

The project required clear documentation of mechanism intent, thermal context, and design trade-offs.

• Contributed to mechanical/thermal design documentation
• Prepared public web visuals from organised images and reports
• Kept large simulation videos out until compressed

1. Mechanism concept

   The work focused on a louver-style mechanism and how controlled motion could support a thermal-control function.

2. Thermal and mechanical context

   Report and presentation figures were used to communicate the thermal-control problem and mechanism layout.

3. Public page preparation

   Selected images and PDFs were included while raw working files and large media stayed outside the website.

Selected project material used to show CAD, component, prototype, or documentation details.

A project page with selected mechanism visuals, thermal-control context, and supporting documentation.

Relevant to mechanical systems design because it connects mechanism layout, thermal-control intent, and documentation.

• Clean portfolio assets should be separated from raw working folders.
• A project page reads better when images are paired with short engineering context.

• Add cleaner rendered screenshots where source CAD or simulation files still need manual export.
• Prepare a dedicated GitHub repository only after source files are cleaned and documented.