Thrust Profile (N)
0.69s Burn WindowEngineered by Cesaroni Technology, the 128G185-12A is a 38mm solid rocket motor designed for model rocketry. As an official G-class motor, it delivers a total impulse of 128.0 Ns over a 0.69 second burn window.
With an average thrust of 183.3 N and a peak of 212.2 N, it features a dual-peak thrust curve optimal for general sport flying. It utilizes the Vmax propellant formulation, dictating its specific impulse and exhaust signature.
Technical Specifications
Canadian Association of RocketryMass Budget
188.4g TotalDesign wings in your spreadsheet
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