Thrust Profile (N)
3.00s Burn WindowEngineered by Cesaroni Technology, the 1364K454-19A is a 54mm solid rocket motor designed for high-power rocketry (HPR). As an official K-class motor, it delivers a total impulse of 1363.7 Ns over a 3.00 second burn window.
With an average thrust of 454.1 N and a peak of 620.0 N, it features a dual-peak thrust curve optimal for general sport flying. It utilizes the Skidmark propellant formulation, dictating its specific impulse and exhaust signature.
Technical Specifications
Canadian Association of RocketryMass Budget
1391g TotalDesign wings in your spreadsheet
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