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