Cesaroni 20146N5800-P

Engineered by Cesaroni Technology, the 20146N5800-P is a 98mm solid rocket motor designed for extreme high-power rocketry. As an official N-class motor, it delivers a total impulse of 20145.7 Ns over a 3.49 second burn window.

With an average thrust of 5774.1 N and a peak of 8034.6 N, it features a dual-peak thrust curve optimal for general sport flying. It utilizes the C-Star propellant formulation, dictating its specific impulse and exhaust signature.