Thrust Profile (N)
1.89s Burn WindowEngineered by Cesaroni Technology, the 108G57-12A is a 29mm solid rocket motor designed for model rocketry. As an official G-class motor, it delivers a total impulse of 107.8 Ns over a 1.89 second burn window.
With an average thrust of 57.2 N and a peak of 85.4 N, it features a regressive thrust curve optimal for general sport flying. It utilizes the Classic propellant formulation, dictating its specific impulse and exhaust signature.
Technical Specifications
Canadian Association of RocketryMass Budget
146g TotalDesign wings in your spreadsheet
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