Thrust Profile (N)
1.89s Burn WindowEngineered by Loki Research, the J670LB is a 54mm solid rocket motor designed for high-power rocketry (HPR). As an official J-class motor, it delivers a total impulse of 1269.8 Ns over a 1.89 second burn window.
With an average thrust of 669.9 N and a peak of 824.1 N, it features a dual-peak thrust curve optimal for general sport flying. It utilizes the Loki Blue propellant formulation, dictating its specific impulse and exhaust signature.
Technical Specifications
Tripoli Rocketry Association, Inc.Mass Budget
1204.2g TotalDesign wings in your spreadsheet
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