Thrust Profile (N)
1.31s Burn WindowEngineered by AeroTech, the J550ST-14 is a 54mm solid rocket motor designed for high-power rocketry (HPR). As an official J-class motor, it delivers a total impulse of 732.0 Ns over a 1.31 second burn window.
With an average thrust of 557.0 N and a peak of 649.0 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
828g TotalDesign wings in your spreadsheet
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