Cesaroni 40960O8000-P

Engineered by Cesaroni Technology, the 40960O8000-P is a 161mm solid rocket motor designed for extreme high-power rocketry. As an official O-class motor, it delivers a total impulse of 40960.0 Ns over a 5.10 second burn window.

With an average thrust of 8034.5 N and a peak of 8605.1 N, it features a regressive thrust curve optimal for sustainer stages and high-altitude attempts. It utilizes the White Thunder propellant formulation, dictating its specific impulse and exhaust signature.