Thrust Profile (N)
2.40s Burn WindowEngineered by Cesaroni Technology, the 1008J420-15A is a 38mm solid rocket motor designed for high-power rocketry (HPR). As an official J-class motor, it delivers a total impulse of 1007.8 Ns over a 2.40 second burn window.
With an average thrust of 419.9 N and a peak of 783.1 N, it features a neutral 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
874g TotalDesign wings in your spreadsheet
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