Thrust Profile (N)
3.20s Burn WindowEngineered by AeroTech, the M2400T is a 98mm solid rocket motor designed for extreme high-power rocketry. As an official M-class motor, it delivers a total impulse of 7716.5 Ns over a 3.20 second burn window.
With an average thrust of 2400.0 N and a peak of 3401.6 N, it features a neutral thrust curve optimal for general sport flying. It utilizes the Blue Thunder propellant formulation, dictating its specific impulse and exhaust signature.
Technical Specifications
Tripoli Rocketry Association, Inc.Mass Budget
6451.2g TotalDesign wings in your spreadsheet
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