Cesaroni 19318N3301-P

Engineered by Cesaroni Technology, the 19318N3301-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 19317.6 Ns over a 5.86 second burn window.

With an average thrust of 3294.3 N and a peak of 5075.7 N, it features a regressive thrust curve optimal for sustainer stages and high-altitude attempts. It utilizes the White propellant formulation, dictating its specific impulse and exhaust signature.