Thrust Profile (N)
2.31s Burn WindowEngineered by Cesaroni Technology, the 819J354-16A is a 38mm solid rocket motor designed for high-power rocketry (HPR). As an official J-class motor, it delivers a total impulse of 818.7 Ns over a 2.31 second burn window.
With an average thrust of 354.7 N and a peak of 521.8 N, it features a regressive thrust curve optimal for general sport flying. It utilizes the White propellant formulation, dictating its specific impulse and exhaust signature.
Technical Specifications
Canadian Association of RocketryMass Budget
778.2g TotalDesign wings in your spreadsheet
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