Thrust Profile (N)
2.66s Burn WindowEngineered by Cesaroni Technology, the 1750K650-16A is a 54mm solid rocket motor designed for high-power rocketry (HPR). As an official K-class motor, it delivers a total impulse of 1749.5 Ns over a 2.66 second burn window.
With an average thrust of 656.0 N and a peak of 728.7 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
1989.9g TotalDesign wings in your spreadsheet
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