Thrust Profile (N)
1.20s Burn WindowEngineered by AeroTech, the J615ST-20A is a 54mm solid rocket motor designed for high-power rocketry (HPR). As an official J-class motor, it delivers a total impulse of 745.5 Ns over a 1.20 second burn window.
With an average thrust of 615.1 N and a peak of 933.9 N, it features a dual-peak thrust curve optimal for general sport flying. It utilizes the Super Thunder propellant formulation, dictating its specific impulse and exhaust signature.
Technical Specifications
Tripoli Rocketry Association, Inc.Mass Budget
801.6999999999999g TotalDesign wings in your spreadsheet
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