Thrust Profile (N)
4.12s Burn WindowEngineered by Cesaroni Technology, the 502I120-15A is a 54mm solid rocket motor designed for high-power rocketry (HPR). As an official I-class motor, it delivers a total impulse of 501.8 Ns over a 4.12 second burn window.
With an average thrust of 122.2 N and a peak of 152.0 N, it features a dual-peak thrust curve optimal for sustainer stages and high-altitude attempts. It utilizes the Imax propellant formulation, dictating its specific impulse and exhaust signature.
Technical Specifications
Canadian Association of RocketryMass Budget
623.2g TotalDesign wings in your spreadsheet
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