Thrust Profile (N)
1.89s Burn WindowEngineered by Cesaroni Technology, the 268H140-11A is a 29mm solid rocket motor designed for high-power rocketry (HPR). As an official H-class motor, it delivers a total impulse of 268.0 Ns over a 1.89 second burn window.
With an average thrust of 141.8 N and a peak of 247.8 N, it features a neutral 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
277g TotalDesign wings in your spreadsheet
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