Thrust Profile (N)
1.03s Burn WindowEngineered by Kosdon by AeroTech, the G135R is a 29mm solid rocket motor designed for model rocketry. As an official G-class motor, it delivers a total impulse of 143.0 Ns over a 1.03 second burn window.
With an average thrust of 137.0 N and a peak of 158.8 N, it features a dual-peak thrust curve optimal for general sport flying. It utilizes the Redline propellant formulation, dictating its specific impulse and exhaust signature.
Technical Specifications
Tripoli Rocketry Association, Inc.Mass Budget
226g TotalDesign wings in your spreadsheet
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