Thrust Profile (N)
1.66s Burn WindowEngineered by Cesaroni Technology, the 999J600-16A is a 38mm solid rocket motor designed for high-power rocketry (HPR). As an official J-class motor, it delivers a total impulse of 998.6 Ns over a 1.66 second burn window.
With an average thrust of 603.5 N and a peak of 721.0 N, it features a dual-peak thrust curve optimal for general sport flying. It utilizes the Red Lightning propellant formulation, dictating its specific impulse and exhaust signature.
Technical Specifications
Tripoli Rocketry Association, Inc.Mass Budget
906g TotalDesign wings in your spreadsheet
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