diff --git a/README.md b/README.md index e4f6f7b..90996b1 100644 --- a/README.md +++ b/README.md @@ -1,20 +1,28 @@ # MANPADS Rocket & Launcher Prototype -[![30 Second Overview](https://img.youtube.com/vi/zFn__6_LdTc/maxresdefault.jpg)](https://www.youtube.com/shorts/zFn__6_LdTc) +## 30 Second Overview -[![Full System Overview (5 min)](https://img.youtube.com/vi/DDO2EvXyncE/maxresdefault.jpg)](https://www.youtube.com/watch?v=DDO2EvXyncE&t=59s) +[![30 Second Overview](https://img.youtube.com/vi/zFn__6_LdTc/hqdefault.jpg)](https://www.youtube.com/shorts/zFn__6_LdTc) + +## Full System Overview (5 Minutes) + +[![Full System Overview](https://img.youtube.com/vi/DDO2EvXyncE/hqdefault.jpg)](https://www.youtube.com/watch?v=DDO2EvXyncE&t=59s) + +--- ## Full Development Media and Documentation https://drive.google.com/drive/folders/17zpks6_R59H0iXJaGkTrtp1SzIFFAQtY?usp=drive_link The Google Drive archive contains additional development media and documentation, including: -- Mechanical design and assembly -- System electronics and firmware testing -- Launch testing and rocket motor development -- System flow diagrams -- Rocket specifications -- Bill of materials and cost breakdown +- Mechanical design and assembly +- System electronics and firmware testing +- Launch testing and rocket motor development +- System flow diagrams +- Rocket specifications +- Bill of materials and cost breakdown + +--- ## Project Overview @@ -26,11 +34,13 @@ The system was designed in Fusion 360, simulated using OpenRocket, and developed The total hardware cost of the prototype is approximately **$96**. +--- + ## Repository Contents This repository contains the core engineering components of the project: -- Mechanical CAD files for the rocket and launcher -- Firmware source code for the rocket flight controller and launcher system -- OpenRocket simulation files used for aerodynamic stability analysis +- Mechanical CAD files for the rocket and launcher +- Firmware source code for the rocket flight controller and launcher system +- OpenRocket simulation files used for aerodynamic stability analysis - Supporting project documentation