Thrust Profile (N)
3.03s Burn WindowEngineered by Cesaroni Technology, the 6287M2075-P is a 75mm solid rocket motor designed for extreme high-power rocketry. As an official M-class motor, it delivers a total impulse of 6286.6 Ns over a 3.03 second burn window.
With an average thrust of 2074.8 N and a peak of 3452.5 N, it features a dual-peak thrust curve optimal for general sport flying. It utilizes the Smoky Sam propellant formulation, dictating its specific impulse and exhaust signature.
Technical Specifications
Canadian Association of RocketryMass Budget
7191g TotalDesign wings in your spreadsheet
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