Thrust Profile (N)
2.19s Burn WindowEngineered by Gorilla Rocket Motors, the J485WC is a 54mm solid rocket motor designed for high-power rocketry (HPR). As an official J-class motor, it delivers a total impulse of 1059.7 Ns over a 2.19 second burn window.
With an average thrust of 484.0 N and a peak of 600.0 N, it features a neutral 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
1190g TotalDesign wings in your spreadsheet
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