Thrust Profile (N)
1.29s Burn WindowEngineered by Cesaroni Technology, the 261H200-14A is a 29mm solid rocket motor designed for high-power rocketry (HPR). As an official H-class motor, it delivers a total impulse of 260.8 Ns over a 1.29 second burn window.
With an average thrust of 201.7 N and a peak of 303.2 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
274g TotalDesign wings in your spreadsheet
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