Thrust Profile (N)
2.10s Burn WindowEngineered by Cesaroni Technology, the 1115J530-15A is a 38mm solid rocket motor designed for high-power rocketry (HPR). As an official J-class motor, it delivers a total impulse of 1115.5 Ns over a 2.10 second burn window.
With an average thrust of 531.2 N and a peak of 828.8 N, it features a neutral thrust curve optimal for general sport flying. It utilizes the Imax propellant formulation, dictating its specific impulse and exhaust signature.
Technical Specifications
Canadian Association of RocketryMass Budget
977g TotalDesign wings in your spreadsheet
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