Thrust Profile (N)
1.17s Burn WindowEngineered by Cesaroni Technology, the 114G100-14A is a 24mm solid rocket motor designed for model rocketry. As an official G-class motor, it delivers a total impulse of 114.5 Ns over a 1.17 second burn window.
With an average thrust of 98.1 N and a peak of 178.8 N, it features a regressive thrust curve optimal for general sport flying. It utilizes the Skidmark propellant formulation, dictating its specific impulse and exhaust signature.
Technical Specifications
Canadian Association of RocketryMass Budget
159g TotalDesign wings in your spreadsheet
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