Thrust Profile (N)
2.26s Burn WindowEngineered by Cesaroni Technology, the 648J285-15A is a 38mm solid rocket motor designed for high-power rocketry (HPR). As an official J-class motor, it delivers a total impulse of 648.0 Ns over a 2.26 second burn window.
With an average thrust of 287.5 N and a peak of 369.3 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
595g TotalDesign wings in your spreadsheet
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