Thrust Profile (N)
2.66s Burn WindowEngineered by Cesaroni Technology, the 1955K735-P is a 75mm solid rocket motor designed for high-power rocketry (HPR). As an official K-class motor, it delivers a total impulse of 1955.2 Ns over a 2.66 second burn window.
With an average thrust of 735.7 N and a peak of 911.0 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
2508.8g TotalDesign wings in your spreadsheet
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