Thrust Profile (N)
0.33s Burn WindowEngineered by Cesaroni Technology, the 25E75-17A is a 24mm solid rocket motor designed for model rocketry. As an official E-class motor, it delivers a total impulse of 24.8 Ns over a 0.33 second burn window.
With an average thrust of 74.3 N and a peak of 99.9 N, it features a dual-peak thrust curve optimal for general sport flying. It utilizes the Vmax propellant formulation, dictating its specific impulse and exhaust signature.
Technical Specifications
Canadian Association of RocketryMass Budget
52g TotalDesign wings in your spreadsheet
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