Thrust Profile (N)
2.33s Burn WindowEngineered by Animal Motor Works, the ST-54-1050 is a 54mm solid rocket motor designed for high-power rocketry (HPR). As an official J-class motor, it delivers a total impulse of 1069.7 Ns over a 2.33 second burn window.
With an average thrust of 459.1 N and a peak of 563.2 N, it features a dual-peak thrust curve optimal for general sport flying. It utilizes the Super Tiger propellant formulation, dictating its specific impulse and exhaust signature.
Technical Specifications
National Association of RocketryMass Budget
1196.4g TotalDesign wings in your spreadsheet
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