Thrust Profile (N)
1.53s Burn WindowEngineered by Cesaroni Technology, the 4807L3150-P is a 98mm solid rocket motor designed for extreme high-power rocketry. As an official L-class motor, it delivers a total impulse of 4807.8 Ns over a 1.53 second burn window.
With an average thrust of 3137.4 N and a peak of 3670.4 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
4731g TotalDesign wings in your spreadsheet
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