Thrust Profile (N)
5.49s Burn WindowEngineered by Cesaroni Technology, the 9870M1800-P is a 98mm solid rocket motor designed for extreme high-power rocketry. As an official M-class motor, it delivers a total impulse of 9869.7 Ns over a 5.49 second burn window.
With an average thrust of 1797.1 N and a peak of 2240.6 N, it features a regressive thrust curve optimal for sustainer stages and high-altitude attempts. It utilizes the Blue Streak propellant formulation, dictating its specific impulse and exhaust signature.
Technical Specifications
Canadian Association of RocketryMass Budget
8342g TotalDesign wings in your spreadsheet
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