Thrust Profile (N)
3.13s Burn WindowEngineered by Cesaroni Technology, the 1994K635-17A is a 54mm solid rocket motor designed for high-power rocketry (HPR). As an official K-class motor, it delivers a total impulse of 1994.4 Ns over a 3.13 second burn window.
With an average thrust of 637.3 N and a peak of 778.7 N, it features a dual-peak thrust curve optimal for general sport flying. It utilizes the Red Lightning propellant formulation, dictating its specific impulse and exhaust signature.
Technical Specifications
Canadian Association of RocketryMass Budget
1768g TotalDesign wings in your spreadsheet
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