Thrust Profile (N)
2.25s Burn WindowEngineered by Loki Research, the J-326-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 732.9 Ns over a 2.25 second burn window.
With an average thrust of 326.2 N and a peak of 925.8 N, it features a regressive thrust curve optimal for heavy rockets requiring high off-the-pad acceleration. It utilizes the Loki Red propellant formulation, dictating its specific impulse and exhaust signature.
Technical Specifications
Tripoli Rocketry Association, Inc.Mass Budget
766g TotalDesign wings in your spreadsheet
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