Thrust Profile (N)
0.85s Burn WindowEngineered by AeroTech, the J1265T is a 54mm solid rocket motor designed for high-power rocketry (HPR). As an official J-class motor, it delivers a total impulse of 1073.3 Ns over a 0.85 second burn window.
With an average thrust of 1261.1 N and a peak of 1745.3 N, it features a regressive thrust curve optimal for general sport flying. It utilizes the Super Thunder propellant formulation, dictating its specific impulse and exhaust signature.
Technical Specifications
Tripoli Rocketry Association, Inc.Mass Budget
1095g TotalDesign wings in your spreadsheet
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