Thrust Profile (N)
1.51s Burn WindowEngineered by Cesaroni Technology, the 2440K1620-P is a 98mm solid rocket motor designed for high-power rocketry (HPR). As an official K-class motor, it delivers a total impulse of 2439.6 Ns over a 1.51 second burn window.
With an average thrust of 1619.5 N and a peak of 1850.9 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
3077g TotalDesign wings in your spreadsheet
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