Thrust Profile (N)
1.34s Burn WindowEngineered by AeroTech, the J575FJ is a 38mm solid rocket motor designed for high-power rocketry (HPR). As an official J-class motor, it delivers a total impulse of 798.1 Ns over a 1.34 second burn window.
With an average thrust of 594.0 N and a peak of 839.5 N, it features a regressive thrust curve optimal for general sport flying. It utilizes the Black Max propellant formulation, dictating its specific impulse and exhaust signature.
Technical Specifications
Tripoli Rocketry Association, Inc.Mass Budget
914g TotalDesign wings in your spreadsheet
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