Thrust Profile (N)
0.96s Burn WindowEngineered by Cesaroni Technology, the 84G88-11A is a 29mm solid rocket motor designed for model rocketry. As an official G-class motor, it delivers a total impulse of 84.3 Ns over a 0.96 second burn window.
With an average thrust of 87.7 N and a peak of 123.6 N, it features a dual-peak thrust curve optimal for general sport flying. It utilizes the Smoky Sam propellant formulation, dictating its specific impulse and exhaust signature.
Technical Specifications
Canadian Association of RocketryMass Budget
152g TotalDesign wings in your spreadsheet
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