Cesaroni 1526K160-6

Engineered by Cesaroni Technology, the 1526K160-6 is a 54mm solid rocket motor designed for high-power rocketry (HPR). As an official K-class motor, it delivers a total impulse of 1525.5 Ns over a 9.66 second burn window.

With an average thrust of 157.9 N and a peak of 282.5 N, it features a dual-peak thrust curve optimal for sustainer stages and high-altitude attempts. It utilizes the Classic propellant formulation, dictating its specific impulse and exhaust signature.