Thrust Profile (N)
2.00s Burn WindowEngineered by Loki Research, the L1400-LW is a 54mm solid rocket motor designed for extreme high-power rocketry. As an official L-class motor, it delivers a total impulse of 2850.6 Ns over a 2.00 second burn window.
With an average thrust of 1400.0 N and a peak of 2710.5 N, it features a neutral 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
2540g TotalDesign wings in your spreadsheet
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