Thrust Profile (N)
1.38s Burn WindowEngineered by Cesaroni Technology, the 207H151-15A is a 29mm solid rocket motor designed for high-power rocketry (HPR). As an official H-class motor, it delivers a total impulse of 207.2 Ns over a 1.38 second burn window.
With an average thrust of 150.8 N and a peak of 214.8 N, it features a regressive thrust curve optimal for general sport flying. It utilizes the Red Lightning propellant formulation, dictating its specific impulse and exhaust signature.
Technical Specifications
Canadian Association of RocketryMass Budget
238g TotalDesign wings in your spreadsheet
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