Thrust Profile (N)
10.76s Burn WindowEngineered by Cesaroni Technology, the 16803N1560-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 16803.0 Ns over a 10.76 second burn window.
With an average thrust of 1561.4 N and a peak of 3216.3 N, it features a neutral thrust curve optimal for heavy rockets requiring high off-the-pad acceleration. It utilizes the White propellant formulation, dictating its specific impulse and exhaust signature.
Technical Specifications
Canadian Association of RocketryMass Budget
15858g TotalDesign wings in your spreadsheet
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