Thrust Profile (N)
8.13s Burn WindowEngineered by Cesaroni Technology, the 4842L610-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 4842.0 Ns over a 8.13 second burn window.
With an average thrust of 613.0 N and a peak of 930.0 N, it features a regressive thrust curve optimal for sustainer stages and high-altitude attempts. It utilizes the Classic propellant formulation, dictating its specific impulse and exhaust signature.
Technical Specifications
Canadian Association of RocketryMass Budget
4975g TotalDesign wings in your spreadsheet
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