Thrust Profile (N)
1.38s Burn WindowEngineered by AeroTech, the M6000ST is a 98mm solid rocket motor designed for extreme high-power rocketry. As an official M-class motor, it delivers a total impulse of 8247.1 Ns over a 1.38 second burn window.
With an average thrust of 5958.9 N and a peak of 6788.7 N, it features a dual-peak thrust curve optimal for general sport flying. It utilizes the Super Thunder propellant formulation, dictating its specific impulse and exhaust signature.
Technical Specifications
Tripoli Rocketry Association, Inc.Mass Budget
8029.6g TotalDesign wings in your spreadsheet
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