Thrust Profile (N)
1.29s Burn WindowEngineered by Cesaroni Technology, the 107G83-14A is a 29mm solid rocket motor designed for model rocketry. As an official G-class motor, it delivers a total impulse of 107.4 Ns over a 1.29 second burn window.
With an average thrust of 83.1 N and a peak of 99.0 N, it features a neutral thrust curve optimal for general sport flying. It utilizes the Blue Streak propellant formulation, dictating its specific impulse and exhaust signature.
Technical Specifications
Canadian Association of RocketryMass Budget
145g TotalDesign wings in your spreadsheet
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