Thrust Profile (N)
1.44s Burn WindowEngineered by Cesaroni Technology, the 258H180-14A is a 29mm solid rocket motor designed for high-power rocketry (HPR). As an official H-class motor, it delivers a total impulse of 258.0 Ns over a 1.44 second burn window.
With an average thrust of 179.6 N and a peak of 266.1 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
314g TotalDesign wings in your spreadsheet
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