Thrust Profile (N)
8.19s Burn WindowEngineered by Cesaroni Technology, the 29920O3700-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 29919.9 Ns over a 8.19 second burn window.
With an average thrust of 3654.3 N and a peak of 4081.6 N, it features a dual-peak thrust curve optimal for sustainer stages and high-altitude attempts. It utilizes the Skidmark propellant formulation, dictating its specific impulse and exhaust signature.
Technical Specifications
Canadian Association of RocketryMass Budget
31350.5g TotalDesign wings in your spreadsheet
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