OSU HART Project 2020-2021
HART's EECS subteam is responsible for all electronics pertaining to the flight of a two stage high powered rocket. The work of several sub teams needs to interface seamlessly during the assembly of the rocket. In order for a successful flight to take place, there must be a system to ignite the booster from a safe distance, and an avionics system in each stage to dictate recovery and ignition events as well as transmit telemetry and track GPS location. While not mission critical, it is paramount that accurate motor performance is recorded during flight to aid in the improvement of the motor design.
1 Lifts 
Artifacts
Name | Description | |
---|---|---|
Project Summary Video | Video summary about our project | Link |
Executive Summary | Executive summary document | Download |
Project Closeout | Project closeout document | Download |
Flight Controller Design | Flight controller design artifacts | Download |
Pressure Transducer | Pressure transducer artifacts | Download |
Launch Communications Transceiver | Launch communications artifacts | Download |
Flight Subsystem | Flight subsystem artifacts | Download |
Launch Controller | Launch system control box artifacts | Download |
Launch Ignition Box | Launch system ignition box artifacts | Download |