Thrust Profile (N)
1.24s Burn WindowEngineered by Cesaroni Technology, the 141G115-13A is a 38mm solid rocket motor designed for model rocketry. As an official G-class motor, it delivers a total impulse of 140.6 Ns over a 1.24 second burn window.
With an average thrust of 113.5 N and a peak of 134.4 N, it features a dual-peak thrust curve optimal for general sport flying. It utilizes the White Thunder propellant formulation, dictating its specific impulse and exhaust signature.
Technical Specifications
Canadian Association of RocketryMass Budget
195g TotalDesign wings in your spreadsheet
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