Thrust Profile (N)
1.93s Burn WindowEngineered by Cesaroni Technology, the 649J335-15A is a 38mm solid rocket motor designed for high-power rocketry (HPR). As an official J-class motor, it delivers a total impulse of 649.2 Ns over a 1.93 second burn window.
With an average thrust of 335.5 N and a peak of 410.6 N, it features a regressive thrust curve optimal for general sport flying. It utilizes the Red Lightning propellant formulation, dictating its specific impulse and exhaust signature.
Technical Specifications
Canadian Association of RocketryMass Budget
627g TotalDesign wings in your spreadsheet
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