Thrust Profile (N)
5.23s Burn WindowEngineered by Cesaroni Technology, the 30600O5800-P is a 161mm solid rocket motor designed for extreme high-power rocketry. As an official O-class motor, it delivers a total impulse of 30605.7 Ns over a 5.23 second burn window.
With an average thrust of 5786.6 N and a peak of 6338.7 N, it features a dual-peak thrust curve optimal for sustainer stages and high-altitude attempts. It utilizes the White Thunder propellant formulation, dictating its specific impulse and exhaust signature.
Technical Specifications
Canadian Association of RocketryMass Budget
26368g TotalDesign wings in your spreadsheet
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