Thrust Profile (N)
2.76s Burn WindowEngineered by Cesaroni Technology, the 127G46-11A is a 38mm solid rocket motor designed for model rocketry. As an official G-class motor, it delivers a total impulse of 127.3 Ns over a 2.76 second burn window.
With an average thrust of 46.2 N and a peak of 112.7 N, it features a dual-peak thrust curve optimal for heavy rockets requiring high off-the-pad acceleration. It utilizes the Classic propellant formulation, dictating its specific impulse and exhaust signature.
Technical Specifications
Canadian Association of RocketryMass Budget
197g TotalDesign wings in your spreadsheet
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