[{"data":1,"prerenderedAt":-1},["ShallowReactive",2],{"project-75101":3},{"id":4,"name":5,"fullName":6,"owner":7,"repo":5,"description":8,"homepage":8,"htmlUrl":8,"language":9,"languages":8,"totalLinesOfCode":8,"stars":10,"forks":11,"watchers":12,"openIssues":13,"contributorsCount":14,"subscribersCount":14,"size":14,"stars1d":15,"stars7d":16,"stars30d":17,"stars90d":14,"forks30d":14,"starsTrendScore":18,"compositeScore":19,"rankGlobal":8,"rankLanguage":8,"license":8,"archived":20,"fork":20,"defaultBranch":21,"hasWiki":22,"hasPages":20,"topics":23,"createdAt":8,"pushedAt":8,"updatedAt":24,"readmeContent":25,"aiSummary":26,"trendingCount":14,"starSnapshotCount":14,"syncStatus":27,"lastSyncTime":28,"discoverSource":29},75101,"MANPADS-System-Launcher-and-Rocket","novatic14\u002FMANPADS-System-Launcher-and-Rocket","novatic14",null,"C++",3776,1058,137,11,0,6,39,96,18,96.17,false,"main",true,[],"2026-06-12 04:01:17","# MANPADS Rocket & Launcher Prototype\n\n## 30 Second Overview\n\n[![30 Second Overview](https:\u002F\u002Fimg.youtube.com\u002Fvi\u002FzFn__6_LdTc\u002Fhqdefault.jpg)](https:\u002F\u002Fwww.youtube.com\u002Fshorts\u002FzFn__6_LdTc)\n\n## Full System Overview (5 Minutes)\n\n[![Full System Overview](https:\u002F\u002Fimg.youtube.com\u002Fvi\u002FDDO2EvXyncE\u002Fhqdefault.jpg)](https:\u002F\u002Fwww.youtube.com\u002Fwatch?v=DDO2EvXyncE&t=59s)\n\n---\n\n## Full Development Media and Documentation\nhttps:\u002F\u002Fdrive.google.com\u002Fdrive\u002Ffolders\u002F17zpks6_R59H0iXJaGkTrtp1SzIFFAQtY?usp=drive_link\n\nThe Google Drive archive contains additional development media and documentation, including:\n\n- Mechanical design and assembly  \n- System electronics and firmware testing  \n- Launch testing and rocket motor development  \n- System flow diagrams  \n- Rocket specifications  \n- Bill of materials and cost breakdown  \n\n---\n\n## Project Overview\n\nThis project is a proof-of-concept prototype of a low-cost rocket launcher and guided rocket system built using consumer electronics and 3D-printed components.\n\nThe rocket uses folding fins and canard stabilization controlled by an onboard ESP32 flight computer and MPU6050 inertial measurement unit. The launcher integrates sensors such as GPS, compass, and barometric modules to determine orientation and provide telemetry.\n\nThe system was designed in Fusion 360, simulated using OpenRocket, and developed through iterative mechanical design, electronics integration, and launch testing.\n\nThe total hardware cost of the prototype is approximately **$96**.\n\n---\n\n## Repository Contents\n\nThis repository contains the core engineering components of the project:\n\n- Mechanical CAD files for the rocket and launcher  \n- Firmware source code for the rocket flight controller and launcher system  \n- OpenRocket simulation files used for aerodynamic stability analysis  \n- Supporting project documentation\n","该项目是一个低成本火箭发射器和制导火箭系统的概念验证原型，使用消费级电子元件和3D打印组件构建。核心功能包括采用折叠翼和前翼稳定设计的火箭，由ESP32飞行计算机和MPU6050惯性测量单元控制；发射器集成了GPS、指南针和气压模块以确定方向并提供遥测数据。项目在Fusion 360中设计，并通过OpenRocket进行仿真，结合了机械设计、电子集成与多次发射测试迭代开发而成。该系统适用于教育演示、小型科研实验以及爱好者自制火箭探索等场景。",2,"2026-06-11 03:52:21","high_star"]