Thrust Profile (N)
1.33s Burn WindowEngineered by Cesaroni Technology, the 311H233-14A is a 29mm solid rocket motor designed for high-power rocketry (HPR). As an official H-class motor, it delivers a total impulse of 311.5 Ns over a 1.33 second burn window.
With an average thrust of 233.5 N and a peak of 354.7 N, it features a dual-peak thrust curve optimal for general sport flying. It utilizes the Red Lightning propellant formulation, dictating its specific impulse and exhaust signature.
Technical Specifications
Canadian Association of RocketryMass Budget
327.6g TotalDesign wings in your spreadsheet
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