Thrust Profile (N)
2.24s Burn WindowEngineered by Cesaroni Technology, the 1013J453-16A is a 38mm solid rocket motor designed for high-power rocketry (HPR). As an official J-class motor, it delivers a total impulse of 1012.6 Ns over a 2.24 second burn window.
With an average thrust of 452.7 N and a peak of 725.3 N, it features a regressive 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
964.3000000000001g TotalDesign wings in your spreadsheet
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