Thrust Profile (N)
3.51s Burn WindowEngineered by AeroTech, the L1300R is a 98mm solid rocket motor designed for extreme high-power rocketry. As an official L-class motor, it delivers a total impulse of 4567.0 Ns over a 3.51 second burn window.
With an average thrust of 1300.0 N and a peak of 1552.0 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
4884g TotalDesign wings in your spreadsheet
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