Imported from GitHub: daedalus-ind/icarus-hardware · commit 44e75af · license MIT

Description

Hardware of the onboard flight computer for the Icarus rocket.

README

Icarus Flight Computer V1.0

This repository contains the hardware design files for the version 1.0 of the flight computer developed for Project Icarus, a model rocket.

📸 Photos

🧰 Overview

The Icarus Flight Computer V1.0 is designed to manage data acquisition, telemetry, and flight event control during rocket missions. The board includes:

• Microcontroller: STMicroelectronics STM32F405RGT6
• 6-Axis IMU: TDK InvenSense ICM-45686
• High-G Accelerometer: Analog Devices ADXL375
• Magnetometer: STMicroelectronics LIS2MDL
• Barometer: MEAS MS5607
• GPS Module: u-blox NEO-M9N
• Radio Module: EBYTE E220-900T22S
• Flash Memory: Windbond W25Q128JV
• E-matches: 2x electric matches for recovery system deployment
• Power Management: TPS631000 buck-boost converter
• Power Supply: 1S LiPo battery or USB-C power input