Thrust Profile (N)
1.63s Burn WindowEngineered by Cesaroni Technology, the 848J520-16A is a 38mm solid rocket motor designed for high-power rocketry (HPR). As an official J-class motor, it delivers a total impulse of 848.4 Ns over a 1.63 second burn window.
With an average thrust of 519.4 N and a peak of 658.2 N, it features a regressive thrust curve optimal for general sport flying. It utilizes the Skidmark propellant formulation, dictating its specific impulse and exhaust signature.
Technical Specifications
Tripoli Rocketry Association, Inc.Mass Budget
850g TotalDesign wings in your spreadsheet
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