Thrust Profile (N)
1.70s Burn WindowEngineered by Loki Research, the G70-CT is a 38mm solid rocket motor designed for model rocketry. As an official G-class motor, it delivers a total impulse of 119.0 Ns over a 1.70 second burn window.
With an average thrust of 70.0 N and a peak of 101.0 N, it features a dual-peak thrust curve optimal for general sport flying. It utilizes the Cocktail propellant formulation, dictating its specific impulse and exhaust signature.
Technical Specifications
Tripoli Rocketry Association, Inc.Mass Budget
242g TotalDesign wings in your spreadsheet
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