Thrust Profile (N)
1.42s Burn WindowEngineered by Gorilla Rocket Motors, the I389GT is a 38mm solid rocket motor designed for high-power rocketry (HPR). As an official I-class motor, it delivers a total impulse of 553.1 Ns over a 1.42 second burn window.
With an average thrust of 389.0 N and a peak of 454.9 N, it features a neutral thrust curve optimal for general sport flying. It utilizes the Green Tornado propellant formulation, dictating its specific impulse and exhaust signature.
Technical Specifications
Tripoli Rocketry Association, Inc.Mass Budget
693g TotalDesign wings in your spreadsheet
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