Thrust Profile (N)
1.22s Burn WindowEngineered by Kosdon by AeroTech, the J520F is a 38mm solid rocket motor designed for high-power rocketry (HPR). As an official J-class motor, it delivers a total impulse of 645.9 Ns over a 1.22 second burn window.
With an average thrust of 525.5 N and a peak of 683.6 N, it features a dual-peak thrust curve optimal for general sport flying. It utilizes the Kosdon Fast propellant formulation, dictating its specific impulse and exhaust signature.
Technical Specifications
Tripoli Rocketry Association, Inc.Mass Budget
722g TotalDesign wings in your spreadsheet
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