Thrust Profile (N)
0.29s Burn WindowEngineered by Cesaroni Technology, the 68F240-15A is a 24mm solid rocket motor designed for model rocketry. As an official F-class motor, it delivers a total impulse of 68.3 Ns over a 0.29 second burn window.
With an average thrust of 236.2 N and a peak of 285.9 N, it features a dual-peak thrust curve optimal for general sport flying. It utilizes the Vmax propellant formulation, dictating its specific impulse and exhaust signature.
Technical Specifications
Canadian Association of RocketryMass Budget
91.8g TotalDesign wings in your spreadsheet
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