Thrust Profile (N)
6.40s Burn WindowEngineered by Cesaroni Technology, the 949J150-P is a 38mm solid rocket motor designed for high-power rocketry (HPR). As an official J-class motor, it delivers a total impulse of 949.2 Ns over a 6.40 second burn window.
With an average thrust of 148.4 N and a peak of 343.2 N, it features a regressive thrust curve optimal for heavy rockets requiring high off-the-pad acceleration. It utilizes the Mellow propellant formulation, dictating its specific impulse and exhaust signature.
Technical Specifications
Canadian Association of RocketryMass Budget
951g TotalDesign wings in your spreadsheet
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