Thrust Profile (N)
3.77s Burn WindowEngineered by Cesaroni Technology, the 2765L730-P is a 54mm solid rocket motor designed for extreme high-power rocketry. As an official L-class motor, it delivers a total impulse of 2765.0 Ns over a 3.77 second burn window.
With an average thrust of 733.0 N and a peak of 1214.8 N, it features a regressive thrust curve optimal for general sport flying. It utilizes the Classic propellant formulation, dictating its specific impulse and exhaust signature.
Technical Specifications
Canadian Association of RocketryMass Budget
2247g TotalDesign wings in your spreadsheet
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