Thrust Profile (N)
2.51s Burn WindowEngineered by Gorilla Rocket Motors, the K555GT is a 54mm solid rocket motor designed for high-power rocketry (HPR). As an official K-class motor, it delivers a total impulse of 1397.0 Ns over a 2.51 second burn window.
With an average thrust of 556.0 N and a peak of 665.5 N, it features a neutral thrust curve optimal for general sport flying. It utilizes the Green Tornado propellant formulation, dictating its specific impulse and exhaust signature.
Technical Specifications
Tripoli Rocketry Association, Inc.Mass Budget
1576.54g TotalDesign wings in your spreadsheet
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