Full Feature Flight Computer
Description
The full feature flight computer is a complete solution for parachute ejection and data logging of high power rocketry flights. The computer is equipped with the base flight computer features such as a barometric pressure sensor for measuring altitude, two pyro ports for dual-deploy recovery, and a USB interface for programming. In addition to these base features, the full feature flight computer contains an IMU for full state measurement using an accelerometer, gyroscope, and magnetometer. The board also contains a high-G accelerometer in order to measure high accelerations during the rocket boost phase. To support staging and redundant ejection setups, the board is equipped with two auxiliary pyro ports that are software configurable.
Technical Specifications
Dimensions: 1.2"x2.9"
Microcontroller: STM32H750VBT6
Processor: ARM Cortex-M7
Maximum Clock Speed: 480 MHz
Memory: 128 kB Flash, 1MB RAM, 4 Mb External Flash
Supply Voltage: 3.6-16V
Maximum Current Draw: 1A
Sensors: Barometric Pressure Sensor, IMU, High-G Accelerometer
Connectivity: USB
Sources and Documentation
Schematic: schematic.pdf
Design Doc: Full-Feature-Flight-Computer-Documentation.pdf
PCB Design Files: GitHub
Firmware Source Code: GitHub
Bill of Materials: BOM.pdf, BOM.xlsx
3D Model: Full-Flight-Computer.step