Thrust Profile (N)
4.60s Burn WindowEngineered by Loki Research, the L840CT is a 76mm solid rocket motor designed for extreme high-power rocketry. As an official L-class motor, it delivers a total impulse of 3889.0 Ns over a 4.60 second burn window.
With an average thrust of 834.0 N and a peak of 1170.0 N, it features a dual-peak thrust curve optimal for sustainer stages and high-altitude attempts. It utilizes the Cocktail propellant formulation, dictating its specific impulse and exhaust signature.
Technical Specifications
Tripoli Rocketry Association, Inc.Mass Budget
3748g TotalDesign wings in your spreadsheet
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