Thrust Profile (N)
1.60s Burn WindowEngineered by Cesaroni Technology, the 217H135-12A is a 29mm solid rocket motor designed for high-power rocketry (HPR). As an official H-class motor, it delivers a total impulse of 216.7 Ns over a 1.60 second burn window.
With an average thrust of 135.1 N and a peak of 171.8 N, it features a regressive thrust curve optimal for general sport flying. It utilizes the White propellant formulation, dictating its specific impulse and exhaust signature.
Technical Specifications
Canadian Association of RocketryMass Budget
251.2g TotalDesign wings in your spreadsheet
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