Thrust Profile (N)
2.87s Burn WindowEngineered by Cesaroni Technology, the 150G50-15A is a 38mm solid rocket motor designed for model rocketry. As an official G-class motor, it delivers a total impulse of 150.0 Ns over a 2.87 second burn window.
With an average thrust of 52.5 N and a peak of 78.8 N, it features a dual-peak thrust curve optimal for general sport flying. It utilizes the Imax propellant formulation, dictating its specific impulse and exhaust signature.
Technical Specifications
Canadian Association of RocketryMass Budget
218g TotalDesign wings in your spreadsheet
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