Thrust Profile (N)
0.85s Burn WindowEngineered by Cesaroni Technology, the 253H295-13A is a 29mm solid rocket motor designed for high-power rocketry (HPR). As an official H-class motor, it delivers a total impulse of 252.7 Ns over a 0.85 second burn window.
With an average thrust of 296.0 N and a peak of 359.5 N, it features a dual-peak thrust curve optimal for general sport flying. It utilizes the Smoky Sam propellant formulation, dictating its specific impulse and exhaust signature.
Technical Specifications
Canadian Association of RocketryMass Budget
342g TotalDesign wings in your spreadsheet
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