Thrust Profile (N)
3.37s Burn WindowEngineered by Cesaroni Technology, the 3147L935-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 3146.8 Ns over a 3.37 second burn window.
With an average thrust of 933.8 N and a peak of 1585.6 N, it features a regressive thrust curve optimal for general sport flying. It utilizes the Imax propellant formulation, dictating its specific impulse and exhaust signature.
Technical Specifications
Canadian Association of RocketryMass Budget
2542g TotalDesign wings in your spreadsheet
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