Thrust Profile (N)
1.07s Burn WindowEngineered by Cesaroni Technology, the 41F36-11A is a 29mm solid rocket motor designed for model rocketry. As an official F-class motor, it delivers a total impulse of 41.2 Ns over a 1.07 second burn window.
With an average thrust of 38.5 N and a peak of 72.7 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
104g TotalDesign wings in your spreadsheet
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