Thrust Profile (N)
3.37s Burn WindowEngineered by Cesaroni Technology, the 1190J355-17A is a 54mm solid rocket motor designed for high-power rocketry (HPR). As an official J-class motor, it delivers a total impulse of 1189.5 Ns over a 3.37 second burn window.
With an average thrust of 353.3 N and a peak of 434.3 N, it features a dual-peak 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
1175g TotalDesign wings in your spreadsheet
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