Thrust Profile (N)
1.27s Burn WindowEngineered by Cesaroni Technology, the 159G125-14A is a 29mm solid rocket motor designed for model rocketry. As an official G-class motor, it delivers a total impulse of 159.6 Ns over a 1.27 second burn window.
With an average thrust of 125.3 N and a peak of 171.8 N, it features a dual-peak thrust curve optimal for general sport flying. It utilizes the Red Lightning propellant formulation, dictating its specific impulse and exhaust signature.
Technical Specifications
Canadian Association of RocketryMass Budget
194.5g TotalDesign wings in your spreadsheet
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