Thrust Profile (N)
3.19s Burn WindowEngineered by Cesaroni Technology, the 518I165-17A is a 54mm solid rocket motor designed for high-power rocketry (HPR). As an official I-class motor, it delivers a total impulse of 512.2 Ns over a 3.19 second burn window.
With an average thrust of 162.6 N and a peak of 190.5 N, it features a dual-peak thrust curve optimal for general sport flying. It utilizes the C-Star propellant formulation, dictating its specific impulse and exhaust signature.
Technical Specifications
Canadian Association of RocketryMass Budget
594g TotalDesign wings in your spreadsheet
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