Thrust Profile (N)
1.08s Burn WindowEngineered by Cesaroni Technology, the 137G127-14A is a 24mm solid rocket motor designed for model rocketry. As an official G-class motor, it delivers a total impulse of 137.3 Ns over a 1.08 second burn window.
With an average thrust of 127.4 N and a peak of 182.1 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
166g TotalDesign wings in your spreadsheet
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