Thrust Profile (N)
4.38s Burn WindowEngineered by Cesaroni Technology, the 143G33-9A is a 29mm solid rocket motor designed for model rocketry. As an official G-class motor, it delivers a total impulse of 143.1 Ns over a 4.38 second burn window.
With an average thrust of 32.7 N and a peak of 66.1 N, it features a dual-peak thrust curve optimal for heavy rockets requiring high off-the-pad acceleration. It utilizes the Mellow 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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