Thrust Profile (N)
1.50s Burn WindowEngineered by Cesaroni Technology, the 75F51-12A is a 24mm solid rocket motor designed for model rocketry. As an official F-class motor, it delivers a total impulse of 75.0 Ns over a 1.50 second burn window.
With an average thrust of 50.0 N and a peak of 85.1 N, it features a dual-peak thrust curve optimal for general sport flying. It utilizes the Classic propellant formulation, dictating its specific impulse and exhaust signature.
Technical Specifications
Canadian Association of RocketryMass Budget
95g TotalDesign wings in your spreadsheet
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