Thrust Profile (N)
1.25s Burn WindowEngineered by Loki Research, the J1000-LW is a 38mm solid rocket motor designed for high-power rocketry (HPR). As an official J-class motor, it delivers a total impulse of 1220.0 Ns over a 1.25 second burn window.
With an average thrust of 976.0 N and a peak of 1400.0 N, it features a regressive thrust curve optimal for general sport flying. It utilizes the Loki White propellant formulation, dictating its specific impulse and exhaust signature.
Technical Specifications
Tripoli Rocketry Association, Inc.Mass Budget
1143g TotalDesign wings in your spreadsheet
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