Thrust Profile (N)
1.81s Burn WindowEngineered by AeroTech, the J460T is a 54mm solid rocket motor designed for high-power rocketry (HPR). As an official J-class motor, it delivers a total impulse of 805.5 Ns over a 1.81 second burn window.
With an average thrust of 460.0 N and a peak of 870.5 N, it features a neutral thrust curve optimal for general sport flying. It utilizes the Blue Thunder propellant formulation, dictating its specific impulse and exhaust signature.
Technical Specifications
Tripoli Rocketry Association, Inc.Mass Budget
789g TotalDesign wings in your spreadsheet
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