Thrust Profile (N)
0.90s Burn WindowEngineered by Kosdon by AeroTech, the J740G is a 38mm solid rocket motor designed for high-power rocketry (HPR). As an official J-class motor, it delivers a total impulse of 682.0 Ns over a 0.90 second burn window.
With an average thrust of 815.0 N and a peak of 956.0 N, it features a neutral thrust curve optimal for general sport flying. It utilizes the Mojave Green propellant formulation, dictating its specific impulse and exhaust signature.
Technical Specifications
Tripoli Rocketry Association, Inc.Mass Budget
724g TotalDesign wings in your spreadsheet
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