Thrust Profile (N)
2.46s Burn WindowEngineered by Cesaroni Technology, the 970J394-13A is a 38mm solid rocket motor designed for high-power rocketry (HPR). As an official J-class motor, it delivers a total impulse of 970.4 Ns over a 2.46 second burn window.
With an average thrust of 394.1 N and a peak of 515.7 N, it features a dual-peak thrust curve optimal for general sport flying. It utilizes the Green3 propellant formulation, dictating its specific impulse and exhaust signature.
Technical Specifications
Canadian Association of RocketryMass Budget
938.9g TotalDesign wings in your spreadsheet
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