Fifth test flight of my R&D project at NARAM58. Aerotech I300T in the booster and Aerotech H123W in the sustainer. Apogee at about 3600 ft. Onboard video was used to validate my gyroscope integration equations. The unit logs data at 400Hz from an analog accelerometer, a digital accelerometer, digital gyroscope, digital barometric pressure sensor, integrated velocity, altitude, pitch, roll, yaw, and 15 different flight events.