Thrust Profile (N)
1.94s Burn WindowEngineered by Cesaroni Technology, the 168H87-12A is a 29mm solid rocket motor designed for high-power rocketry (HPR). As an official H-class motor, it delivers a total impulse of 167.9 Ns over a 1.94 second burn window.
With an average thrust of 86.7 N and a peak of 139.2 N, it features a dual-peak thrust curve optimal for general sport flying. It utilizes the Imax propellant formulation, dictating its specific impulse and exhaust signature.
Technical Specifications
Canadian Association of RocketryMass Budget
205g TotalDesign wings in your spreadsheet
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