Thrust Profile (N)
0.77s Burn WindowEngineered by Cesaroni Technology, the 53F70-14A is a 24mm solid rocket motor designed for model rocketry. As an official F-class motor, it delivers a total impulse of 52.9 Ns over a 0.77 second burn window.
With an average thrust of 69.1 N and a peak of 97.0 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
73g TotalDesign wings in your spreadsheet
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