Thrust Profile (N)
5.25s Burn WindowEngineered by Cesaroni Technology, the 9876M1890-P is a 98mm solid rocket motor designed for extreme high-power rocketry. As an official M-class motor, it delivers a total impulse of 9875.6 Ns over a 5.25 second burn window.
With an average thrust of 1889.0 N and a peak of 2401.6 N, it features a dual-peak thrust curve optimal for sustainer stages and high-altitude attempts. It utilizes the Red Lightning propellant formulation, dictating its specific impulse and exhaust signature.
Technical Specifications
Canadian Association of RocketryMass Budget
8823g TotalDesign wings in your spreadsheet
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