Thrust Profile (N)
1.40s Burn WindowEngineered by Cesaroni Technology, the 220H160-14A is a 29mm solid rocket motor designed for high-power rocketry (HPR). As an official H-class motor, it delivers a total impulse of 220.5 Ns over a 1.40 second burn window.
With an average thrust of 159.0 N and a peak of 191.9 N, it features a dual-peak thrust curve optimal for general sport flying. It utilizes the Skidmark propellant formulation, dictating its specific impulse and exhaust signature.
Technical Specifications
Canadian Association of RocketryMass Budget
272g TotalDesign wings in your spreadsheet
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