Thrust Profile (N)
3.00s Burn WindowEngineered by Loki Research, the M3000-LW is a 76mm solid rocket motor designed for extreme high-power rocketry. As an official M-class motor, it delivers a total impulse of 8838.0 Ns over a 3.00 second burn window.
With an average thrust of 2946.0 N and a peak of 4780.0 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
7160g TotalDesign wings in your spreadsheet
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