Thrust Profile (N)
0.86s Burn WindowEngineered by Cesaroni Technology, the 68F79-13A is a 24mm solid rocket motor designed for model rocketry. As an official F-class motor, it delivers a total impulse of 67.8 Ns over a 0.86 second burn window.
With an average thrust of 78.8 N and a peak of 98.3 N, it features a regressive thrust curve optimal for general sport flying. It utilizes the Smoky Sam propellant formulation, dictating its specific impulse and exhaust signature.
Technical Specifications
Canadian Association of RocketryMass Budget
107.5g TotalDesign wings in your spreadsheet
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