Thrust Profile (N)
0.41s Burn WindowEngineered by Cesaroni Technology, the 168H410-14A is a 29mm solid rocket motor designed for high-power rocketry (HPR). As an official H-class motor, it delivers a total impulse of 167.7 Ns over a 0.41 second burn window.
With an average thrust of 409.0 N and a peak of 522.8 N, it features a neutral thrust curve optimal for general sport flying. It utilizes the Vmax propellant formulation, dictating its specific impulse and exhaust signature.
Technical Specifications
Canadian Association of RocketryMass Budget
182.5g TotalDesign wings in your spreadsheet
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