Thrust Profile (N)
2.08s Burn WindowEngineered by Cesaroni Technology, the 654J316-17A is a 38mm solid rocket motor designed for high-power rocketry (HPR). As an official J-class motor, it delivers a total impulse of 654.3 Ns over a 2.08 second burn window.
With an average thrust of 315.1 N and a peak of 448.7 N, it features a regressive thrust curve optimal for general sport flying. It utilizes the Pink propellant formulation, dictating its specific impulse and exhaust signature.
Technical Specifications
Canadian Association of RocketryMass Budget
607.1g TotalDesign wings in your spreadsheet
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