Cesaroni 2406K555-P

Engineered by Cesaroni Technology, the 2406K555-P is a 75mm solid rocket motor designed for high-power rocketry (HPR). As an official K-class motor, it delivers a total impulse of 2406.2 Ns over a 4.33 second burn window.

With an average thrust of 555.1 N and a peak of 646.7 N, it features a dual-peak thrust curve optimal for sustainer stages and high-altitude attempts. It utilizes the White propellant formulation, dictating its specific impulse and exhaust signature.