Thrust Profile (N)
2.97s Burn WindowEngineered by Cesaroni Technology, the 4025L1355-P is a 75mm solid rocket motor designed for extreme high-power rocketry. As an official L-class motor, it delivers a total impulse of 4025.5 Ns over a 2.97 second burn window.
With an average thrust of 1355.7 N and a peak of 1792.2 N, it features a neutral thrust curve optimal for general sport flying. It utilizes the Smoky Sam propellant formulation, dictating its specific impulse and exhaust signature.
Technical Specifications
Canadian Association of RocketryMass Budget
4962g TotalDesign wings in your spreadsheet
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