Thrust Profile (N)
1.84s Burn WindowEngineered by AeroTech, the J340M is a 38mm solid rocket motor designed for high-power rocketry (HPR). As an official J-class motor, it delivers a total impulse of 651.7 Ns over a 1.84 second burn window.
With an average thrust of 354.1 N and a peak of 605.0 N, it features a regressive thrust curve optimal for general sport flying. It utilizes the Metalstorm propellant formulation, dictating its specific impulse and exhaust signature.
Technical Specifications
Tripoli Rocketry Association, Inc.Mass Budget
577.3g TotalDesign wings in your spreadsheet
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