Thrust Profile (N)
1.30s Burn WindowEngineered by Cesaroni Technology, the 139G107-12A is a 24mm solid rocket motor designed for model rocketry. As an official G-class motor, it delivers a total impulse of 139.1 Ns over a 1.30 second burn window.
With an average thrust of 106.9 N and a peak of 230.7 N, it features a regressive thrust curve optimal for heavy rockets requiring high off-the-pad acceleration. It utilizes the White Thunder propellant formulation, dictating its specific impulse and exhaust signature.
Technical Specifications
Canadian Association of RocketryMass Budget
169.8g TotalDesign wings in your spreadsheet
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