Thrust Profile (N)
4.47s Burn WindowEngineered by Cesaroni Technology, the 14200N3180-P is a 98mm solid rocket motor designed for extreme high-power rocketry. As an official N-class motor, it delivers a total impulse of 14200.1 Ns over a 4.47 second burn window.
With an average thrust of 3179.3 N and a peak of 3770.0 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
12198g TotalDesign wings in your spreadsheet
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