Thrust Profile (N)
1.65s Burn WindowEngineered by Cesaroni Technology, the 985J595-16A is a 38mm solid rocket motor designed for high-power rocketry (HPR). As an official J-class motor, it delivers a total impulse of 985.0 Ns over a 1.65 second burn window.
With an average thrust of 595.4 N and a peak of 925.4 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
866g TotalDesign wings in your spreadsheet
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