Thrust Profile (N)
3.24s Burn WindowEngineered by AeroTech, the L1420R is a 75mm solid rocket motor designed for extreme high-power rocketry. As an official L-class motor, it delivers a total impulse of 4603.0 Ns over a 3.24 second burn window.
With an average thrust of 1420.0 N and a peak of 1814.0 N, it features a dual-peak thrust curve optimal for general sport flying. It utilizes the Redline propellant formulation, dictating its specific impulse and exhaust signature.
Technical Specifications
Tripoli Rocketry Association, Inc.Mass Budget
4562g TotalDesign wings in your spreadsheet
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Install in Google Sheets coming soonBB-75-2500
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