Thrust Profile (N)
0.90s Burn WindowEngineered by Cesaroni Technology, the 229H255-14A is a 29mm solid rocket motor designed for high-power rocketry (HPR). As an official H-class motor, it delivers a total impulse of 229.3 Ns over a 0.90 second burn window.
With an average thrust of 254.3 N and a peak of 363.0 N, it features a neutral thrust curve optimal for general sport flying. It utilizes the White Thunder propellant formulation, dictating its specific impulse and exhaust signature.
Technical Specifications
Canadian Association of RocketryMass Budget
232g TotalDesign wings in your spreadsheet
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