Thrust Profile (N)
19.81s Burn WindowEngineered by AeroTech, the G8ST is a 29mm solid rocket motor designed for model rocketry. As an official G-class motor, it delivers a total impulse of 130.0 Ns over a 19.81 second burn window.
With an average thrust of 6.6 N and a peak of 7.8 N, it features a dual-peak thrust curve optimal for sustainer stages and high-altitude attempts. It utilizes the Super Thunder propellant formulation, dictating its specific impulse and exhaust signature.
Technical Specifications
Tripoli Rocketry Association, Inc.Mass Budget
157.1g TotalDesign wings in your spreadsheet
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