Thrust Profile (N)
0.45s Burn WindowEngineered by Cesaroni Technology, the 110G250-14A is a 29mm solid rocket motor designed for model rocketry. As an official G-class motor, it delivers a total impulse of 110.0 Ns over a 0.45 second burn window.
With an average thrust of 243.7 N and a peak of 288.3 N, it features a dual-peak thrust curve optimal for general sport flying. It utilizes the Vmax propellant formulation, dictating its specific impulse and exhaust signature.
Technical Specifications
Canadian Association of RocketryMass Budget
141.3g TotalDesign wings in your spreadsheet
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