Thrust Profile (N)
6.23s Burn WindowEngineered by Cesaroni Technology, the 614I100-17A is a 54mm solid rocket motor designed for high-power rocketry (HPR). As an official I-class motor, it delivers a total impulse of 613.6 Ns over a 6.23 second burn window.
With an average thrust of 98.5 N and a peak of 358.4 N, it features a regressive thrust curve optimal for heavy rockets requiring high off-the-pad acceleration. It utilizes the Red Lightning propellant formulation, dictating its specific impulse and exhaust signature.
Technical Specifications
Canadian Association of RocketryMass Budget
807g TotalDesign wings in your spreadsheet
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