Thrust Profile (N)
2.15s Burn WindowEngineered by Loki Research, the J320-LR is a 38mm solid rocket motor designed for high-power rocketry (HPR). As an official J-class motor, it delivers a total impulse of 720.9 Ns over a 2.15 second burn window.
With an average thrust of 335.0 N and a peak of 550.9 N, it features a regressive thrust curve optimal for general sport flying. It utilizes the Loki Red propellant formulation, dictating its specific impulse and exhaust signature.
Technical Specifications
Tripoli Rocketry Association, Inc.Mass Budget
752g TotalDesign wings in your spreadsheet
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