Thrust Profile (N)
0.88s Burn WindowEngineered by Cesaroni Technology, the 206H237-13A is a 29mm solid rocket motor designed for high-power rocketry (HPR). As an official H-class motor, it delivers a total impulse of 206.2 Ns over a 0.88 second burn window.
With an average thrust of 237.2 N and a peak of 295.9 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
294g TotalDesign wings in your spreadsheet
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