Thrust Profile (N)
1.21s Burn WindowEngineered by Cesaroni Technology, the 273H225-14A is a 38mm solid rocket motor designed for high-power rocketry (HPR). As an official H-class motor, it delivers a total impulse of 273.2 Ns over a 1.21 second burn window.
With an average thrust of 226.3 N and a peak of 254.1 N, it features a dual-peak 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
193g TotalDesign wings in your spreadsheet
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