Thrust Profile (N)
2.15s Burn WindowEngineered by Cesaroni Technology, the 266H125-12A is a 38mm solid rocket motor designed for high-power rocketry (HPR). As an official H-class motor, it delivers a total impulse of 285.6 Ns over a 2.15 second burn window.
With an average thrust of 125.1 N and a peak of 152.9 N, it features a dual-peak thrust curve optimal for general sport flying. It utilizes the Classic propellant formulation, dictating its specific impulse and exhaust signature.
Technical Specifications
Canadian Association of RocketryMass Budget
293g TotalDesign wings in your spreadsheet
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