Thrust Profile (N)
0.96s Burn WindowEngineered by Cesaroni Technology, the 57F59-12A is a 29mm solid rocket motor designed for model rocketry. As an official F-class motor, it delivers a total impulse of 57.0 Ns over a 0.96 second burn window.
With an average thrust of 58.9 N and a peak of 70.9 N, it features a dual-peak thrust curve optimal for general sport flying. It utilizes the White Thunder propellant formulation, dictating its specific impulse and exhaust signature.
Technical Specifications
Canadian Association of RocketryMass Budget
99g TotalDesign wings in your spreadsheet
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