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Supaero Space Section
Rocket Avionics.
Avionics for a 9,000 m-apogee competition rocket
Flight computer, sensors and telemetry for a student competition rocket designed to reach a 9,000 m apogee.
With the Supaero Space Section, the student space club at ISAE-SUPAERO, I’m part of the team building a competition rocket designed to reach an apogee of 9,000 m.
As an avionics engineer I designed and tested the avionics subsystem — flight computer, sensors and telemetry — and managed its hardware/software integration, with a focus on reliability under high-g launch conditions.
Highlights
- 01Avionics subsystem design: flight computer, sensors and telemetry
- 02Hardware/software integration
- 03Reliability under high-g launch conditions
- 04Subsystem testing