Thrust Profile (N)
1.31s Burn WindowEngineered by Cesaroni Technology, the 30795O25000-P is a 132mm solid rocket motor designed for extreme high-power rocketry. As an official O-class motor, it delivers a total impulse of 30794.0 Ns over a 1.31 second burn window.
With an average thrust of 23507.0 N and a peak of 29275.0 N, it features a regressive thrust curve optimal for general sport flying. It utilizes the Vmax propellant formulation, dictating its specific impulse and exhaust signature.
Technical Specifications
Canadian Association of RocketryMass Budget
23558g TotalDesign wings in your spreadsheet
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