Thrust Profile (N)
1.84s Burn WindowEngineered by Cesaroni Technology, the 784J425-16A is a 38mm solid rocket motor designed for high-power rocketry (HPR). As an official J-class motor, it delivers a total impulse of 783.9 Ns over a 1.84 second burn window.
With an average thrust of 426.9 N and a peak of 631.0 N, it features a regressive thrust curve optimal for general sport flying. It utilizes the Blue Streak propellant formulation, dictating its specific impulse and exhaust signature.
Technical Specifications
Tripoli Rocketry Association, Inc.Mass Budget
700g TotalDesign wings in your spreadsheet
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