Thrust Profile (N)
1.75s Burn WindowEngineered by Cesaroni Technology, the 117G69-14A is a 38mm solid rocket motor designed for model rocketry. As an official G-class motor, it delivers a total impulse of 121.1 Ns over a 1.75 second burn window.
With an average thrust of 69.2 N and a peak of 103.9 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
197g TotalDesign wings in your spreadsheet
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