Thrust Profile (N)
2.97s Burn WindowEngineered by Cesaroni Technology, the 159G54-12A is a 29mm solid rocket motor designed for model rocketry. As an official G-class motor, it delivers a total impulse of 159.1 Ns over a 2.97 second burn window.
With an average thrust of 53.6 N and a peak of 119.2 N, it features a dual-peak thrust curve optimal for heavy rockets requiring high off-the-pad acceleration. It utilizes the Red Lightning propellant formulation, dictating its specific impulse and exhaust signature.
Technical Specifications
Canadian Association of RocketryMass Budget
192.8g TotalDesign wings in your spreadsheet
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