Thrust Profile (N)
2.23s Burn WindowEngineered by AeroTech, the L1940X is a 75mm solid rocket motor designed for extreme high-power rocketry. As an official L-class motor, it delivers a total impulse of 4329.2 Ns over a 2.23 second burn window.
With an average thrust of 1939.3 N and a peak of 2318.5 N, it features a regressive thrust curve optimal for general sport flying. It utilizes the Propellant X propellant formulation, dictating its specific impulse and exhaust signature.
Technical Specifications
Tripoli Rocketry Association, Inc.Mass Budget
3855.5g TotalDesign wings in your spreadsheet
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Install in Google Sheets coming soonBB-75-2500
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