Thrust Profile (N)
3.35s Burn WindowEngineered by Cesaroni Technology, the 2377K711-18A is a 54mm solid rocket motor designed for high-power rocketry (HPR). As an official K-class motor, it delivers a total impulse of 2377.3 Ns over a 3.35 second burn window.
With an average thrust of 710.4 N and a peak of 1700.6 N, it features a regressive thrust curve optimal for heavy rockets requiring high off-the-pad acceleration. It utilizes the White propellant formulation, dictating its specific impulse and exhaust signature.
Technical Specifications
Canadian Association of RocketryMass Budget
2198g TotalDesign wings in your spreadsheet
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