Thrust Profile (N)
2.32s Burn WindowEngineered by AeroTech, the M2225WS is a 75mm solid rocket motor designed for extreme high-power rocketry. As an official M-class motor, it delivers a total impulse of 5205.0 Ns over a 2.32 second burn window.
With an average thrust of 2239.2 N and a peak of 2418.4 N, it features a dual-peak thrust curve optimal for general sport flying. It utilizes the Super White Lightning propellant formulation, dictating its specific impulse and exhaust signature.
Technical Specifications
Tripoli Rocketry Association, Inc.Mass Budget
4695g TotalDesign wings in your spreadsheet
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