Thrust Profile (N)
1.67s Burn WindowEngineered by Cesaroni Technology, the 53F32-12A is a 29mm solid rocket motor designed for model rocketry. As an official F-class motor, it delivers a total impulse of 52.8 Ns over a 1.67 second burn window.
With an average thrust of 31.6 N and a peak of 49.3 N, it features a dual-peak thrust curve optimal for general sport flying. It utilizes the White propellant formulation, dictating its specific impulse and exhaust signature.
Technical Specifications
Canadian Association of RocketryMass Budget
107g TotalDesign wings in your spreadsheet
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