Thrust Profile (N)
1.00s Burn WindowEngineered by AeroTech, the G104T is a 29mm solid rocket motor designed for model rocketry. As an official G-class motor, it delivers a total impulse of 81.5 Ns over a 1.00 second burn window.
With an average thrust of 104.0 N and a peak of 113.8 N, it features a regressive 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
136g TotalDesign wings in your spreadsheet
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