Thrust Profile (N)
1.24s Burn WindowEngineered by Cesaroni Technology, the 315H255-14A is a 29mm solid rocket motor designed for high-power rocketry (HPR). As an official H-class motor, it delivers a total impulse of 315.4 Ns over a 1.24 second burn window.
With an average thrust of 254.2 N and a peak of 411.1 N, it features a neutral 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
318g TotalDesign wings in your spreadsheet
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