Thrust Profile (N)
3.12s Burn WindowEngineered by Cesaroni Technology, the 168H54-10A is a 29mm solid rocket motor designed for high-power rocketry (HPR). As an official H-class motor, it delivers a total impulse of 167.7 Ns over a 3.12 second burn window.
With an average thrust of 53.8 N and a peak of 105.0 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
209g TotalDesign wings in your spreadsheet
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