Thrust Profile (N)
2.12s Burn WindowEngineered by Cesaroni Technology, the 2412K1085-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 2412.0 Ns over a 2.12 second burn window.
With an average thrust of 1113.0 N and a peak of 1204.0 N, it features a dual-peak thrust curve optimal for general sport flying. It utilizes the White Thunder propellant formulation, dictating its specific impulse and exhaust signature.
Technical Specifications
Canadian Association of RocketryMass Budget
2430g TotalDesign wings in your spreadsheet
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