Thrust Profile (N)
2.26s Burn WindowEngineered by Cesaroni Technology, the 765J330-16A is a 38mm solid rocket motor designed for high-power rocketry (HPR). As an official J-class motor, it delivers a total impulse of 765.0 Ns over a 2.26 second burn window.
With an average thrust of 325.3 N and a peak of 459.3 N, it features a regressive 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
702g TotalDesign wings in your spreadsheet
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