Thrust Profile (N)
1.44s Burn WindowEngineered by Cesaroni Technology, the 176H123-12A is a 29mm solid rocket motor designed for high-power rocketry (HPR). As an official H-class motor, it delivers a total impulse of 176.5 Ns over a 1.44 second burn window.
With an average thrust of 123.0 N and a peak of 149.8 N, it features a progressive 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
228g TotalDesign wings in your spreadsheet
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