Thrust Profile (N)
6.16s Burn WindowEngineered by Cesaroni Technology, the 21062O3400-P is a 98mm solid rocket motor designed for extreme high-power rocketry. As an official O-class motor, it delivers a total impulse of 21062.2 Ns over a 6.16 second burn window.
With an average thrust of 3416.7 N and a peak of 4750.3 N, it features a dual-peak thrust curve optimal for sustainer stages and high-altitude attempts. It utilizes the Imax propellant formulation, dictating its specific impulse and exhaust signature.
Technical Specifications
Canadian Association of RocketryMass Budget
16842g TotalDesign wings in your spreadsheet
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