Thrust Profile (N)
1.20s Burn WindowEngineered by Gorilla Rocket Motors, the I392BL is a 38mm solid rocket motor designed for high-power rocketry (HPR). As an official I-class motor, it delivers a total impulse of 416.1 Ns over a 1.20 second burn window.
With an average thrust of 392.0 N and a peak of 508.2 N, it features a thrust curve optimal for general sport flying. It utilizes the Black Lightning propellant formulation, dictating its specific impulse and exhaust signature.
Technical Specifications
Tripoli Rocketry Association, Inc.Mass Budget
657g TotalDesign wings in your spreadsheet
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