Thrust Profile (N)
5.94s Burn WindowEngineered by Gorilla Rocket Motors, the K222WC is a 54mm solid rocket motor designed for high-power rocketry (HPR). As an official K-class motor, it delivers a total impulse of 1314.5 Ns over a 5.94 second burn window.
With an average thrust of 221.6 N and a peak of 444.4 N, it features a dual-peak thrust curve optimal for heavy rockets requiring high off-the-pad acceleration. It utilizes the White Cloud propellant formulation, dictating its specific impulse and exhaust signature.
Technical Specifications
Tripoli Rocketry Association, Inc.Mass Budget
1596.54g TotalDesign wings in your spreadsheet
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