Thrust Profile (N)
1.22s Burn WindowEngineered by Cesaroni Technology, the 142G117-11A is a 24mm solid rocket motor designed for model rocketry. As an official G-class motor, it delivers a total impulse of 142.3 Ns over a 1.22 second burn window.
With an average thrust of 116.8 N and a peak of 181.2 N, it features a regressive thrust curve optimal for general sport flying. It utilizes the White propellant formulation, dictating its specific impulse and exhaust signature.
Technical Specifications
Canadian Association of RocketryMass Budget
172.5g TotalDesign wings in your spreadsheet
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