Cesaroni 13766N2500-P

Engineered by Cesaroni Technology, the 13766N2500-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 13766.0 Ns over a 5.38 second burn window.

With an average thrust of 2562.0 N and a peak of 3875.8 N, it features a regressive thrust curve optimal for sustainer stages and high-altitude attempts. It utilizes the Classic propellant formulation, dictating its specific impulse and exhaust signature.