Thrust Profile (N)
1.90s Burn WindowEngineered by Cesaroni Technology, the 232H123-14A is a 38mm solid rocket motor designed for high-power rocketry (HPR). As an official H-class motor, it delivers a total impulse of 232.4 Ns over a 1.90 second burn window.
With an average thrust of 122.5 N and a peak of 153.3 N, it features a dual-peak thrust curve optimal for general sport flying. It utilizes the Skidmark propellant formulation, dictating its specific impulse and exhaust signature.
Technical Specifications
Canadian Association of RocketryMass Budget
297g TotalDesign wings in your spreadsheet
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