Thrust Profile (N)
3.18s Burn WindowEngineered by Cesaroni Technology, the 465I150-11A is a 54mm solid rocket motor designed for high-power rocketry (HPR). As an official I-class motor, it delivers a total impulse of 465.1 Ns over a 3.18 second burn window.
With an average thrust of 149.5 N and a peak of 179.2 N, it features a dual-peak thrust curve optimal for general sport flying. It utilizes the Blue Streak propellant formulation, dictating its specific impulse and exhaust signature.
Technical Specifications
Tripoli Rocketry Association, Inc.Mass Budget
570g TotalDesign wings in your spreadsheet
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