Thrust Profile (N)
3.35s Burn WindowEngineered by Cesaroni Technology, the 806J240-16A is a 54mm solid rocket motor designed for high-power rocketry (HPR). As an official J-class motor, it delivers a total impulse of 806.0 Ns over a 3.35 second burn window.
With an average thrust of 240.8 N and a peak of 299.4 N, it features a dual-peak thrust curve optimal for general sport flying. It utilizes the Red Lightning propellant formulation, dictating its specific impulse and exhaust signature.
Technical Specifications
Canadian Association of RocketryMass Budget
875g TotalDesign wings in your spreadsheet
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