Thrust Profile (N)
1.89s Burn WindowEngineered by Cesaroni Technology, the 774J410-16A is a 38mm solid rocket motor designed for high-power rocketry (HPR). As an official J-class motor, it delivers a total impulse of 773.8 Ns over a 1.89 second burn window.
With an average thrust of 408.9 N and a peak of 512.1 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
735g TotalDesign wings in your spreadsheet
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