The Spring-Powered Parachute Ejection Avionics Bay is an integrated recovery and electronics module designed for small experimental rockets, educational rocket projects, and student-built launch vehicles.

This module combines a spring-powered parachute ejection system with a dedicated PCB mounting area, allowing users to house their avionics while also supporting a mechanical parachute deployment structure.

Rather than functioning only as an electronics enclosure, this avionics bay is designed to support both flight electronics integration and recovery system deployment in a single compact module. The internal structure can provide space for a flight computer, sensors, battery, wiring, and parachute storage depending on the project configuration.

Because each rocket may require a different body diameter, PCB size, parachute volume, spring force, and internal layout, this product may be customized based on project requirements.

Included Components

• Spring-powered parachute ejection avionics bay body

• Parachute storage compartment

• Spring-powered ejection structure

• Internal PCB mounting space

• Basic internal support structure

• Rocket body integration structure