Cesaroni 17907N2540-P

Engineered by Cesaroni Technology, the 17907N2540-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 17907.0 Ns over a 7.04 second burn window.

With an average thrust of 2543.4 N and a peak of 2915.3 N, it features a dual-peak thrust curve optimal for sustainer stages and high-altitude attempts. It utilizes the Green3 propellant formulation, dictating its specific impulse and exhaust signature.