Thrust Profile (N)
2.25s Burn WindowEngineered by Cesaroni Technology, the 491I218-14A is a 54mm solid rocket motor designed for high-power rocketry (HPR). As an official I-class motor, it delivers a total impulse of 491.2 Ns over a 2.25 second burn window.
With an average thrust of 218.3 N and a peak of 294.2 N, it features a dual-peak thrust curve optimal for general sport flying. It utilizes the White Thunder propellant formulation, dictating its specific impulse and exhaust signature.
Technical Specifications
Tripoli Rocketry Association, Inc.Mass Budget
580g TotalDesign wings in your spreadsheet
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