Thrust Profile (N)
1.27s Burn WindowEngineered by Cesaroni Technology, the 217H170-14A is a 29mm solid rocket motor designed for high-power rocketry (HPR). As an official H-class motor, it delivers a total impulse of 217.1 Ns over a 1.27 second burn window.
With an average thrust of 171.3 N and a peak of 243.8 N, it features a dual-peak thrust curve optimal for general sport flying. It utilizes the Blue Streak 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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