Thrust Profile (N)
1.55s Burn WindowEngineered by Cesaroni Technology, the 896J580-17A is a 38mm solid rocket motor designed for high-power rocketry (HPR). As an official J-class motor, it delivers a total impulse of 896.4 Ns over a 1.55 second burn window.
With an average thrust of 577.4 N and a peak of 691.5 N, it features a regressive thrust curve optimal for general sport flying. It utilizes the Smoky Sam propellant formulation, dictating its specific impulse and exhaust signature.
Technical Specifications
Tripoli Rocketry Association, Inc.Mass Budget
1044g TotalDesign wings in your spreadsheet
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