Cesaroni 2486K510-P

Engineered by Cesaroni Technology, the 2486K510-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 2486.0 Ns over a 4.84 second burn window.

With an average thrust of 514.0 N and a peak of 689.8 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.