Thrust Profile (N)
1.15s Burn WindowEngineered by Gorilla Rocket Motors, the J607WC is a 38mm solid rocket motor designed for high-power rocketry (HPR). As an official J-class motor, it delivers a total impulse of 677.9 Ns over a 1.15 second burn window.
With an average thrust of 607.0 N and a peak of 803.6 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
824g TotalDesign wings in your spreadsheet
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