Thrust Profile (N)
1.31s Burn WindowEngineered by Cesaroni Technology, the 138G106-14A is a 29mm solid rocket motor designed for model rocketry. As an official G-class motor, it delivers a total impulse of 138.3 Ns over a 1.31 second burn window.
With an average thrust of 106.0 N and a peak of 128.7 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
187g TotalDesign wings in your spreadsheet
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