Thrust Profile (N)
1.84s Burn WindowEngineered by Kosdon by AeroTech, the I301W is a 38mm solid rocket motor designed for high-power rocketry (HPR). As an official I-class motor, it delivers a total impulse of 554.0 Ns over a 1.84 second burn window.
With an average thrust of 302.0 N and a peak of 433.0 N, it features a dual-peak thrust curve optimal for general sport flying. It utilizes the White Lightning propellant formulation, dictating its specific impulse and exhaust signature.
Technical Specifications
National Association of RocketryMass Budget
725.5g TotalDesign wings in your spreadsheet
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