Thrust Profile (N)
3.52s Burn WindowEngineered by Gorilla Rocket Motors, the K670WC is a 75mm solid rocket motor designed for high-power rocketry (HPR). As an official K-class motor, it delivers a total impulse of 2364.7 Ns over a 3.52 second burn window.
With an average thrust of 670.0 N and a peak of 859.1 N, it features a thrust curve optimal for general sport flying. It utilizes the White Cloud propellant formulation, dictating its specific impulse and exhaust signature.
Technical Specifications
Tripoli Rocketry Association, Inc.Mass Budget
2706g TotalDesign wings in your spreadsheet
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