Thrust Profile (N)
4.28s Burn WindowEngineered by Cesaroni Technology, the 2772L640-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 2772.2 Ns over a 4.28 second burn window.
With an average thrust of 638.4 N and a peak of 1590.0 N, it features a regressive thrust curve optimal for heavy rockets requiring high off-the-pad acceleration. It utilizes the Classic/Dual Thrust propellant formulation, dictating its specific impulse and exhaust signature.
Technical Specifications
Canadian Association of RocketryMass Budget
2244g TotalDesign wings in your spreadsheet
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