Thrust Profile (N)
1.19s Burn WindowEngineered by Cesaroni Technology, the 60F50-13A is a 24mm solid rocket motor designed for model rocketry. As an official F-class motor, it delivers a total impulse of 59.7 Ns over a 1.19 second burn window.
With an average thrust of 50.0 N and a peak of 69.9 N, it features a regressive thrust curve optimal for general sport flying. It utilizes the Skidmark propellant formulation, dictating its specific impulse and exhaust signature.
Technical Specifications
Canadian Association of RocketryMass Budget
93.9g TotalDesign wings in your spreadsheet
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