Thrust Profile (N)
1.14s Burn WindowEngineered by Cesaroni Technology, the 2330K2000-P is a 75mm solid rocket motor designed for high-power rocketry (HPR). As an official K-class motor, it delivers a total impulse of 2329.9 Ns over a 1.14 second burn window.
With an average thrust of 2036.1 N and a peak of 2480.9 N, it features a dual-peak thrust curve optimal for general sport flying. It utilizes the Vmax propellant formulation, dictating its specific impulse and exhaust signature.
Technical Specifications
Canadian Association of RocketryMass Budget
2464.5g TotalDesign wings in your spreadsheet
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