Thrust Profile (N)
2.82s Burn WindowEngineered by Cesaroni Technology, the 286H100-15A is a 38mm solid rocket motor designed for high-power rocketry (HPR). As an official H-class motor, it delivers a total impulse of 286.4 Ns over a 2.82 second burn window.
With an average thrust of 101.7 N and a peak of 117.9 N, it features a dual-peak thrust curve optimal for general sport flying. It utilizes the Imax propellant formulation, dictating its specific impulse and exhaust signature.
Technical Specifications
Canadian Association of RocketryMass Budget
327g TotalDesign wings in your spreadsheet
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