Thrust Profile (N)
3.52s Burn WindowEngineered by Cesaroni Technology, the 1281K360-13A is a 54mm solid rocket motor designed for high-power rocketry (HPR). As an official K-class motor, it delivers a total impulse of 1280.9 Ns over a 3.52 second burn window.
With an average thrust of 363.6 N and a peak of 405.5 N, it features a neutral thrust curve optimal for general sport flying. It utilizes the White propellant formulation, dictating its specific impulse and exhaust signature.
Technical Specifications
Canadian Association of RocketryMass Budget
1232g TotalDesign wings in your spreadsheet
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