Thrust Profile (N)
1.83s Burn WindowEngineered by Cesaroni Technology, the 216H118-12A is a 29mm solid rocket motor designed for high-power rocketry (HPR). As an official H-class motor, it delivers a total impulse of 216.2 Ns over a 1.83 second burn window.
With an average thrust of 118.4 N and a peak of 191.3 N, it features a regressive thrust curve optimal for general sport flying. It utilizes the Classic propellant formulation, dictating its specific impulse and exhaust signature.
Technical Specifications
Canadian Association of RocketryMass Budget
232g TotalDesign wings in your spreadsheet
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