Thrust Profile (N)
1.15s Burn WindowEngineered by AeroTech, the J825R is a 38mm solid rocket motor designed for high-power rocketry (HPR). As an official J-class motor, it delivers a total impulse of 974.9 Ns over a 1.15 second burn window.
With an average thrust of 892.9 N and a peak of 1244.3 N, it features a regressive thrust curve optimal for general sport flying. It utilizes the Redline propellant formulation, dictating its specific impulse and exhaust signature.
Technical Specifications
Tripoli Rocketry Association, Inc.Mass Budget
875g TotalDesign wings in your spreadsheet
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