Thrust Profile (N)
6.87s Burn WindowEngineered by Cesaroni Technology, the 9955M1450-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 9955.0 Ns over a 6.87 second burn window.
With an average thrust of 1456.0 N and a peak of 2416.3 N, it features a regressive thrust curve optimal for sustainer stages and high-altitude attempts. It utilizes the Classic propellant formulation, dictating its specific impulse and exhaust signature.
Technical Specifications
Canadian Association of RocketryMass Budget
8578g TotalDesign wings in your spreadsheet
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