Thrust Profile (N)
9.91s Burn WindowEngineered by Cesaroni Technology, the 2645L265-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 2644.6 Ns over a 9.91 second burn window.
With an average thrust of 266.8 N and a peak of 471.1 N, it features a regressive thrust curve optimal for sustainer stages and high-altitude attempts. It utilizes the Mellow propellant formulation, dictating its specific impulse and exhaust signature.
Technical Specifications
Canadian Association of RocketryMass Budget
2481g TotalDesign wings in your spreadsheet
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