Thrust Profile (N)
1.34s Burn WindowEngineered by Cesaroni Technology, the 260H194-14A is a 29mm solid rocket motor designed for high-power rocketry (HPR). As an official H-class motor, it delivers a total impulse of 260.3 Ns over a 1.34 second burn window.
With an average thrust of 194.3 N and a peak of 292.0 N, it features a dual-peak thrust curve optimal for general sport flying. It utilizes the Red Lightning propellant formulation, dictating its specific impulse and exhaust signature.
Technical Specifications
Canadian Association of RocketryMass Budget
284g TotalDesign wings in your spreadsheet
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