Thrust Profile (N)
1.78s Burn WindowEngineered by Cesaroni Technology, the 56F31-12A is a 29mm solid rocket motor designed for model rocketry. As an official F-class motor, it delivers a total impulse of 55.5 Ns over a 1.78 second burn window.
With an average thrust of 31.1 N and a peak of 65.0 N, it features a dual-peak thrust curve optimal for heavy rockets requiring high off-the-pad acceleration. It utilizes the Classic propellant formulation, dictating its specific impulse and exhaust signature.
Technical Specifications
Canadian Association of RocketryMass Budget
102g TotalDesign wings in your spreadsheet
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