Thrust Profile (N)
9.10s Burn WindowEngineered by Gorilla Rocket Motors, the K235WC is a 75mm solid rocket motor designed for high-power rocketry (HPR). As an official K-class motor, it delivers a total impulse of 2074.3 Ns over a 9.10 second burn window.
With an average thrust of 235.0 N and a peak of 428.2 N, it features a thrust curve optimal for sustainer stages and high-altitude attempts. It utilizes the White Cloud propellant formulation, dictating its specific impulse and exhaust signature.
Technical Specifications
Tripoli Rocketry Association, Inc.Mass Budget
2770g TotalDesign wings in your spreadsheet
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