Commercial Solid Rocket Motor
Cesaroni Pro29, with no onboard electronic control
Weber was developed in three distinct variants, each crafted to collect critical flight data. The mission was to validate our in-house flight simulator, Gladys, and provide our newest team members with hands-on experience in both rocket design and real-world launch operation.
Additionally, the Weber campaign supported attempts to obtain the Level 1 (L1) high-power rocketry certification, a qualification that authorizes individuals to fly high-power rocket motors within a defined impulse range.
For the three versions, the deployment system is carried out using a motor delay ejection followed by the deployment of a single parachute, a solution widely used when no avionics are available and for small rockets.
Although Weber did not incorporate active flight control avionics, it carried a payload exclusively intended to obtain flight data, which constitutes its independent system.
It consists only of the MissileWorks RRC3 commercial avionics device that allows velocity and altitude data to be recorded throughout the flight. It is powered by a battery and switched on or off via a switch.
It is important to note that this system was used strictly for data acquisition and did not perform deployment control or flight actuation functions.