Thrust Profile (N)
1.00s Burn WindowEngineered by Cesaroni Technology, the 50F51-13A is a 24mm solid rocket motor designed for model rocketry. As an official F-class motor, it delivers a total impulse of 49.9 Ns over a 1.00 second burn window.
With an average thrust of 49.6 N and a peak of 69.4 N, it features a regressive thrust curve optimal for general sport flying. It utilizes the Blue Streak 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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