Thrust Profile (N)
2.67s Burn WindowEngineered by Cesaroni Technology, the 1412K530-16A is a 54mm solid rocket motor designed for high-power rocketry (HPR). As an official K-class motor, it delivers a total impulse of 1412.0 Ns over a 2.67 second burn window.
With an average thrust of 529.0 N and a peak of 596.4 N, it features a dual-peak thrust curve optimal for general sport flying. It utilizes the Smoky Sam propellant formulation, dictating its specific impulse and exhaust signature.
Technical Specifications
Canadian Association of RocketryMass Budget
1639.8g TotalDesign wings in your spreadsheet
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