Thrust Profile (N)
5.89s Burn WindowEngineered by Cesaroni Technology, the 10367N1800-P is a 98mm solid rocket motor designed for extreme high-power rocketry. As an official N-class motor, it delivers a total impulse of 10366.9 Ns over a 5.89 second burn window.
With an average thrust of 1759.8 N and a peak of 2216.4 N, it features a regressive thrust curve optimal for sustainer stages and high-altitude attempts. It utilizes the White propellant formulation, dictating its specific impulse and exhaust signature.
Technical Specifications
Canadian Association of RocketryMass Budget
9180g TotalDesign wings in your spreadsheet
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