Thrust Profile (N)
2.90s Burn WindowEngineered by Cesaroni Technology, the 2383K820-17A is a 54mm solid rocket motor designed for high-power rocketry (HPR). As an official K-class motor, it delivers a total impulse of 2383.0 Ns over a 2.90 second burn window.
With an average thrust of 821.6 N and a peak of 1470.6 N, it features a regressive thrust curve optimal for general sport flying. It utilizes the Blue Streak propellant formulation, dictating its specific impulse and exhaust signature.
Technical Specifications
Canadian Association of RocketryMass Budget
1982g TotalDesign wings in your spreadsheet
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