Thrust Profile (N)
1.20s Burn WindowEngineered by Gorilla Rocket Motors, the I462WC is a 38mm solid rocket motor designed for high-power rocketry (HPR). As an official I-class motor, it delivers a total impulse of 556.7 Ns over a 1.20 second burn window.
With an average thrust of 462.0 N and a peak of 557.1 N, it features a thrust curve optimal for general sport flying. It utilizes the White Cloud propellant formulation, dictating its specific impulse and exhaust signature.
Technical Specifications
Tripoli Rocketry Association, Inc.Mass Budget
678g TotalDesign wings in your spreadsheet
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