Thrust Profile (N)
1.02s Burn WindowEngineered by Cesaroni Technology, the 166H163-14A is a 29mm solid rocket motor designed for high-power rocketry (HPR). As an official H-class motor, it delivers a total impulse of 166.3 Ns over a 1.02 second burn window.
With an average thrust of 162.7 N and a peak of 216.9 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
187g TotalDesign wings in your spreadsheet
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