Thrust Profile (N)
0.85s Burn WindowEngineered by Cesaroni Technology, the 26E31-15A is a 24mm solid rocket motor designed for model rocketry. As an official E-class motor, it delivers a total impulse of 26.1 Ns over a 0.85 second burn window.
With an average thrust of 30.8 N and a peak of 52.6 N, it features a regressive 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
52g TotalDesign wings in your spreadsheet
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