Thrust Profile (N)
0.71s Burn WindowEngineered by Cesaroni Technology, the 282H399-12A is a 29mm solid rocket motor designed for high-power rocketry (HPR). As an official H-class motor, it delivers a total impulse of 282.2 Ns over a 0.71 second burn window.
With an average thrust of 399.3 N and a peak of 545.8 N, it features a dual-peak thrust curve optimal for general sport flying. It utilizes the White Thunder 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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